Started by upstream project "gplibrary_PR_Models" build number 86 originally caused by: GitHub pull request #165 of commit f08d0abb912431f7fa14d583dd199557c0f2e32a, no merge conflicts. Building remotely on reynolds in workspace /jenkins/workspace/gplibrary_PR_Models/mosek Wiping out workspace first. Cloning the remote Git repository Cloning repository https://github.com/convexengineering/gplibrary > git init /jenkins/workspace/gplibrary_PR_Models/mosek # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git --version # timeout=10 > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/heads/*:refs/remotes/origin/* > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 > git config --add remote.origin.fetch +refs/heads/*:refs/remotes/origin/* # timeout=10 > git config remote.origin.url https://github.com/convexengineering/gplibrary # timeout=10 Fetching upstream changes from https://github.com/convexengineering/gplibrary > git fetch --tags --progress https://github.com/convexengineering/gplibrary +refs/pull/*:refs/remotes/origin/pr/* +refs/heads/master:refs/remotes/origin/master Merging Revision a7764a21dff699d3c7f74e09f50361a18c36fcff (refs/remotes/origin/pr/165/merge) to origin/master, UserMergeOptions{mergeRemote='origin', mergeTarget='master', mergeStrategy='default', fastForwardMode='--ff'} > git rev-parse origin/master^{commit} # timeout=10 > git config core.sparsecheckout # timeout=10 > git checkout -f origin/master # timeout=3 > git merge --ff a7764a21dff699d3c7f74e09f50361a18c36fcff # timeout=10 > git rev-parse HEAD^{commit} # timeout=10 Seen branch in repository origin/1682literate Seen branch in repository origin/1682master Seen branch in repository origin/Breakdown Seen branch in repository origin/SPaircraft Seen branch in repository origin/aerosurf Seen branch in repository origin/atmosphere Seen branch in repository origin/bounds5 Seen branch in repository origin/boxspar Seen branch in repository origin/breguet_range Seen branch in repository origin/breguetsetup Seen branch in repository origin/climb Seen branch in repository origin/commercial_sizing Seen branch in repository origin/d8 Seen branch in repository origin/d8fuselage Seen branch 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Run condition [Execution node ] enabling prebuild for step [Execute shell] Run condition [Execution node ] enabling prebuild for step [Execute Windows batch command] [description-setter] Description set: PR 165: Multiple blade element model [Execution node] check if [reynolds] is in [[macys, macys_VM, reynolds, reynolds-ubuntu16]] Run condition [Execution node ] enabling perform for step [Execute shell] [mosek] $ /bin/bash -xe /tmp/jenkins8094871683115397205.sh + [[ reynolds == *macys* ]] + virtualenv /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit New python executable in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/python Installing setuptools, pip, wheel...done. + . /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/activate ++ deactivate nondestructive ++ unset -f pydoc ++ '[' -z '' ']' ++ '[' -z '' ']' ++ '[' -n /bin/bash ']' ++ hash -r ++ '[' -z '' ']' ++ unset VIRTUAL_ENV ++ '[' '!' nondestructive = nondestructive ']' ++ VIRTUAL_ENV=/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit ++ export VIRTUAL_ENV ++ _OLD_VIRTUAL_PATH=/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games ++ PATH=/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games ++ export PATH ++ '[' -z '' ']' ++ '[' -z '' ']' ++ _OLD_VIRTUAL_PS1= ++ '[' x '!=' x ']' +++ basename /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit ++ PS1='(venv2_gpkit) ' ++ export PS1 ++ alias pydoc ++ '[' -n /bin/bash ']' ++ hash -r ++ which pip + export PIP=/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip + PIP=/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pip Requirement already up-to-date: pip in ./venv2_gpkit/lib/python2.7/site-packages (10.0.1) + [[ reynolds == *reynolds* ]] + export CVXOPT_SUITESPARSE_INC_DIR=/usr/include/suitesparse + CVXOPT_SUITESPARSE_INC_DIR=/usr/include/suitesparse + export PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games + PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games + [[ mosek == mosek ]] + [[ reynolds == reynolds-ubuntu16 ]] + export PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/home/jenkins/mosek/7/tools/platform/linux64x86/bin + PATH=/home/jenkins/.local/bin/:/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin:/usr/local/sbin:/usr/local/bin:/usr/sbin:/usr/bin:/sbin:/bin:/usr/games:/usr/local/games:/home/jenkins/mosek/7/tools/platform/linux64x86/bin + python /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/setup.py install running install running build running build_py running install_lib creating /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib.linux-x86_64-2.7/mosek/__init__.py -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying build/lib.linux-x86_64-2.7/mosek/array.py -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek creating /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/fusion/__init__.py -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/fusion/Utils.py -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion copying build/lib.linux-x86_64-2.7/mosek/fusion/SolverInfo.py -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion byte-compiling /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/__init__.py to __init__.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/array.py to array.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/__init__.py to __init__.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/Utils.py to Utils.pyc byte-compiling /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek/fusion/SolverInfo.py to SolverInfo.pyc running install_data copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosek64.so.7.1 -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libiomp5.so -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosekxx7_1.so -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../bin/libmosekglb64.so.7.1 -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek copying /home/jenkins/mosek/7/tools/platform/linux64x86/python/2/../../../../../license.pdf -> /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/mosek running install_egg_info Writing /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages/Mosek-7.1.20-py2.7.egg-info Please review the MOSEK license conditions in license.pdf + [[ mosek == mosek ]] + python -c '__import__("mosek").Env()' + msktestlic Computer Platform : Linux/64-X86 Cores : 20 Problem Name : Objective sense : min Type : LO (linear optimization problem) Constraints : 1 Cones : 0 Scalar variables : 5000 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator - tries : 0 time : 0.00 Eliminator - elim's : 0 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.00 Interior-point optimizer terminated. Time: 0.00. Optimizer terminated. Time: 0.03 ************************************ A license was checked out correctly. ************************************ + export 'GPKITSOLVERS=mosek, mosek_cli' + GPKITSOLVERS='mosek, mosek_cli' + [[ mosek == cvxopt ]] + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade xmlrunner Collecting xmlrunner Installing collected packages: xmlrunner Successfully installed xmlrunner-1.7.7 + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pint Collecting pint Installing collected packages: pint Successfully installed pint-0.8.1 + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade numpy Collecting numpy Using cached https://files.pythonhosted.org/packages/76/4d/418dda252cf92bad00ab82d6b2a856e7843b47a5c2f084aed34b14b67d64/numpy-1.14.2-cp27-cp27mu-manylinux1_x86_64.whl Installing collected packages: numpy Successfully installed numpy-1.14.2 + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade scipy Collecting scipy Using cached https://files.pythonhosted.org/packages/9c/0b/5deb712a9ea5bb0a1de837d04ef7625c5f3ee44efe7ed0765ceda681d7f1/scipy-1.0.1-cp27-cp27mu-manylinux1_x86_64.whl Requirement not upgraded as not directly required: numpy>=1.8.2 in ./venv2_gpkit/lib/python2.7/site-packages (from scipy) (1.14.2) Installing collected packages: scipy Successfully installed scipy-1.0.1 + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade ctypesgen Collecting ctypesgen Installing collected packages: ctypesgen Successfully installed ctypesgen-0.post125 + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade pandas Collecting pandas Using cached https://files.pythonhosted.org/packages/6b/b5/76538d8a202f8c368d30c18892d33664d1a3b2c078af8513ee5b5d172629/pandas-0.22.0-cp27-cp27mu-manylinux1_x86_64.whl Collecting python-dateutil (from pandas) Using cached https://files.pythonhosted.org/packages/0c/57/19f3a65bcf6d5be570ee8c35a5398496e10a0ddcbc95393b2d17f86aaaf8/python_dateutil-2.7.2-py2.py3-none-any.whl Requirement not upgraded as not directly required: numpy>=1.9.0 in ./venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2) Collecting pytz>=2011k (from pandas) Using cached https://files.pythonhosted.org/packages/dc/83/15f7833b70d3e067ca91467ca245bae0f6fe56ddc7451aa0dc5606b120f2/pytz-2018.4-py2.py3-none-any.whl Collecting six>=1.5 (from python-dateutil->pandas) Using cached https://files.pythonhosted.org/packages/67/4b/141a581104b1f6397bfa78ac9d43d8ad29a7ca43ea90a2d863fe3056e86a/six-1.11.0-py2.py3-none-any.whl Installing collected packages: six, python-dateutil, pytz, pandas Successfully installed pandas-0.22.0 python-dateutil-2.7.2 pytz-2018.4 six-1.11.0 + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --upgrade matplotlib Collecting matplotlib Using cached https://files.pythonhosted.org/packages/33/da/6409d32c46778ed20308e83bc501ff2ff8a9cbda5dd7b26362c5e99a6149/matplotlib-2.2.2-cp27-cp27mu-manylinux1_x86_64.whl Collecting pyparsing!=2.0.4,!=2.1.2,!=2.1.6,>=2.0.1 (from matplotlib) Using cached https://files.pythonhosted.org/packages/6a/8a/718fd7d3458f9fab8e67186b00abdd345b639976bc7fb3ae722e1b026a50/pyparsing-2.2.0-py2.py3-none-any.whl Collecting backports.functools-lru-cache (from matplotlib) Using cached https://files.pythonhosted.org/packages/03/8e/2424c0e65c4a066e28f539364deee49b6451f8fcd4f718fefa50cc3dcf48/backports.functools_lru_cache-1.5-py2.py3-none-any.whl Collecting subprocess32 (from matplotlib) Requirement not upgraded as not directly required: pytz in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2018.4) Requirement not upgraded as not directly required: six>=1.10 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.11.0) Requirement not upgraded as not directly required: python-dateutil>=2.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (2.7.2) Collecting kiwisolver>=1.0.1 (from matplotlib) Using cached https://files.pythonhosted.org/packages/3a/62/a8c9bef3059d55ab38e41fe9cba4fad773bfc04e47290bab84db1c18262e/kiwisolver-1.0.1-cp27-cp27mu-manylinux1_x86_64.whl Collecting cycler>=0.10 (from matplotlib) Using cached https://files.pythonhosted.org/packages/f7/d2/e07d3ebb2bd7af696440ce7e754c59dd546ffe1bbe732c8ab68b9c834e61/cycler-0.10.0-py2.py3-none-any.whl Requirement not upgraded as not directly required: numpy>=1.7.1 in ./venv2_gpkit/lib/python2.7/site-packages (from matplotlib) (1.14.2) Requirement not upgraded as not directly required: setuptools in ./venv2_gpkit/lib/python2.7/site-packages (from kiwisolver>=1.0.1->matplotlib) (39.0.1) Installing collected packages: pyparsing, backports.functools-lru-cache, subprocess32, kiwisolver, cycler, matplotlib Successfully installed backports.functools-lru-cache-1.5 cycler-0.10.0 kiwisolver-1.0.1 matplotlib-2.2.2 pyparsing-2.2.0 subprocess32-3.2.7 + export GPKITBUILD=/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit + GPKITBUILD=/jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit + python -c 'import scipy; print scipy.__version__' 1.0.1 + python -c 'import numpy; print numpy.__version__' 1.14.2 + python -c 'import pint; print pint.__version__' 0.8.1 + git clone --depth 1 https://github.com/convexengineering/gpkit.git Cloning into 'gpkit'... + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Obtaining file:///jenkins/workspace/gplibrary_PR_Models/mosek/gpkit Requirement already satisfied: numpy>=1.12.1 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (1.14.2) Requirement already satisfied: pint>=0.7 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (0.8.1) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkit==0.7.0.0) (1.0.1) Collecting ad (from gpkit==0.7.0.0) Downloading https://files.pythonhosted.org/packages/3b/f0/16776411190d53745d0d020a242e2890a59c0752b133a3476d35aa63e4a2/ad-1.3.2.zip Installing collected packages: ad, gpkit Running setup.py install for ad: started Running setup.py install for ad: finished with status 'done' Running setup.py develop for gpkit Successfully installed ad-1.3.2 gpkit + python /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip install --no-cache-dir -e /jenkins/workspace/gplibrary_PR_Models/mosek Obtaining file:///jenkins/workspace/gplibrary_PR_Models/mosek Requirement already satisfied: numpy>=1.12 in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in ./venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1) Installing collected packages: gpkitmodels Running setup.py develop for gpkitmodels Successfully installed gpkitmodels + cat /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit/gpkit/env/settings installed_solvers : mosek, mosek_cli mosek_bin_dir : /home/jenkins/mosek/7/tools/platform/linux64x86/bin + ls /jenkins/workspace/gplibrary_PR_Models/mosek/build_gpkit expopt.so + export MSK_IPAR_NUM_THREADS=2 + MSK_IPAR_NUM_THREADS=2 + export MKL_NUM_THREADS=2 + MKL_NUM_THREADS=2 + export NUMEXPR_NUM_THREADS=2 + NUMEXPR_NUM_THREADS=2 + export OMP_NUM_THREADS=2 + OMP_NUM_THREADS=2 + python -c 'from gpkit.tests.test_repo import test_repos; test_repos(xmloutput=True, ingpkitmodels=True)' Obtaining file:///jenkins/workspace/gplibrary_PR_Models/mosek Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Not uninstalling gpkitmodels at /jenkins/workspace/gplibrary_PR_Models/mosek, outside environment /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit Can't uninstall 'gpkitmodels'. No files were found to uninstall. Running setup.py develop for gpkitmodels Successfully installed gpkitmodels Cloning into 'shopping'... Running tests... ---------------------------------------------------------------------- ... ---------------------------------------------------------------------- Ran 3 tests in 0.631s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.141 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0366 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.231 seconds. Cloning into 'gassolar'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-req-build-d_Rxhe Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-vB1Q1l/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Installing collected packages: gpfit Successfully installed gpfit-0.1 Processing /jenkins/workspace/gplibrary_PR_Models/mosek/gassolar Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-lJlMMo/wheels/95/3b/d6/ef583514b36970c50f7f7fc39ef6c0801ca762afbdc19fb0cd Successfully built gassolar Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 Running tests... ---------------------------------------------------------------------- ../jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 26.282s OK Generating XML reports... adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 592 variables. Solving took 0.341 seconds. Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Beginning signomial solve. Solving took 4 GP solves and 0.925 seconds. Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 592 variables. Solving took 0.213 seconds. Warning: Variable [P_{shaft-max}_Mission/Climb/FlightSegment/AircraftPerf/EnginePerf_(0,)**-1*P_{total}_Mission/Climb/ could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Beginning signomial solve. Solving took 4 GP solves and 1.1 seconds. Warning: Variable [P_{shaft-max}_Mission.1/Climb.1/FlightSegment.2/AircraftPerf.2/EnginePerf.2_(0,)**-1*P_{total}_Miss could cause inaccurate result because it is above upper bound. Solution is 1.0000 but bound is 0.9685 Using solver 'mosek' Solving for 1250 variables. Solving took 0.353 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.1496 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.1345 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 2.1 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0581 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.9086 but bound is 150000.0000 Using solver 'mosek_cli' Solving for 1250 variables. Solving took 0.533 seconds. Warning: Variable Re_Mission/FlightSegment/AircraftPerf/WingAero could cause inaccurate result because it is below lower bound. Solution is 131551.0147 but bound is 150000.0000 Warning: Variable Re_Mission/FlightSegment.10/AircraftPerf.10/WingAero.10 could cause inaccurate result because it is below lower bound. Solution is 131552.3302 but bound is 150000.0000 Beginning signomial solve. Solving took 4 GP solves and 3.38 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134552.5355 but bound is 150000.0000 Warning: Variable Re_Mission.1/FlightSegment.21/AircraftPerf.21/WingAero.21 could cause inaccurate result because it is below lower bound. Solution is 134553.8810 but bound is 150000.0000 Cloning into 'jho'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-req-build-6o1DXx Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-N0okZQ/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Running tests... ---------------------------------------------------------------------- ...adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -5.050126983263681e-14. Allowing negative dual variable(s) as small as -7.590672881918614e-14. Allowing negative dual variable(s) as small as -1.5105191403241847e-13. Allowing negative dual variable(s) as small as -1.4975260614891184e-13. Solving took 4 GP solves and 2.83 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0065420559297635e-14. Allowing negative dual variable(s) as small as -7.408396812680351e-14. Allowing negative dual variable(s) as small as -1.5029123778820264e-13. Allowing negative dual variable(s) as small as -1.49964242412981e-13. Solving took 4 GP solves and 2.89 seconds. Allowing negative dual variable(s) as small as -5.183093537697303e-13. Allowing negative dual variable(s) as small as -1.4299846029519614e-12. Allowing negative dual variable(s) as small as -4.4411002653177434e-13. Allowing negative dual variable(s) as small as -4.4534341492319385e-13. Allowing negative dual variable(s) as small as -1.296652889226646e-12. Allowing negative dual variable(s) as small as -1.091077532142104e-12. Allowing negative dual variable(s) as small as -1.0907750397359806e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -2.6935918773229872e-15. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.6323134905121117e-14. Allowing negative dual variable(s) as small as -5.695990546995736e-12. Allowing negative dual variable(s) as small as -2.0878980496915973e-11. Allowing negative dual variable(s) as small as -2.0880920619396563e-11. Solving took 4 GP solves and 3.02 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.81 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.155962462533026e-13. Allowing negative dual variable(s) as small as -1.429564799870775e-12. Allowing negative dual variable(s) as small as -4.45107492530461e-13. Allowing negative dual variable(s) as small as -4.447033019605584e-13. Allowing negative dual variable(s) as small as -1.296481043182307e-12. Allowing negative dual variable(s) as small as -1.0922071623856167e-12. Allowing negative dual variable(s) as small as -1.0929329273198785e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.7433970933566911e-16. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.4087889072699903e-14. Allowing negative dual variable(s) as small as -5.695981004904887e-12. Allowing negative dual variable(s) as small as -2.0878942246231564e-11. Allowing negative dual variable(s) as small as -2.088071071287965e-11. Solving took 4 GP solves and 2.77 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.. ---------------------------------------------------------------------- Ran 4 tests in 40.779s OK Generating XML reports... 71 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Cloning into 'turbofan'... Processing /jenkins/workspace/gplibrary_PR_Models/mosek/turbofan Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.8.1) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-15xR7u/wheels/05/a3/bb/c109a767ce427bad8712257bfeb944703a233ba8210a5b0c35 Successfully built turbofan Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 1.753s OK Generating XML reports... adding test for 'turbofan/engine_validation.py' Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(0,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(0,) [N]...] is not tight because the left hand side evaluated to 24184.7528315 newton but the right hand side evaluated to 24184.16 newton (Allowable error: 0.0001%, Actual error: 0.0025%) Warning: Constraint [F_{6}_Engine/EnginePerformance/ThrustPerformance_(1,) + F_{8}_Engine/EnginePerformance/ThrustPerform... >= F_Engine/EnginePerformance/ThrustPerformance_(1,) [N]...] is not tight because the left hand side evaluated to 26232.8485055 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Cloning into 'SPaircraft'... Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to /tmp/pip-req-build-gU3YYa Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (1.0.1) Requirement already satisfied: pint in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from turbofan==0.0.0.0) (0.8.1) Building wheels for collected packages: turbofan Running setup.py bdist_wheel for turbofan: started Running setup.py bdist_wheel for turbofan: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-pefmi0/wheels/49/e6/3a/5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan Running tests... ---------------------------------------------------------------------- adding test for 'SP_aircraft.py' Solving over 9 passes. Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2519604.41527 force_pound * meter but the right hand side evaluated to 2468460.42372 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4850654 force_pound but the right hand side evaluated to 32399.9999988 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116795 meter but the right hand side evaluated to 1.96396091051 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(0, 0) [N]...] is not tight because the left hand side evaluated to 48608.8106948 newton but the right hand side evaluated to 48529.6547271 newton (Allowable error: 0.1%, Actual error: 0.16%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(1, 0) [N]...] is not tight because the left hand side evaluated to 49704.4483099 newton but the right hand side evaluated to 49411.2154445 newton (Allowable error: 0.1%, Actual error: 0.59%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(3, 0) [N]...] is not tight because the left hand side evaluated to 18949.0210128 newton but the right hand side evaluated to 18923.024418 newton (Allowable error: 0.1%, Actual error: 0.14%) Warning: Constraint [F_{6}_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) + F_{8}_Mission/Aircraft/En... >= F_Mission/Aircraft/Engine/EnginePerformance/ThrustPerformance_(4, 0) [N]...] is not tight because the left hand side evaluated to 16591.9573078 newton but the right hand side evaluated to 16565.7489631 newton (Allowable error: 0.1%, Actual error: 0.16%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1002816.64491 joule / kilogram but the right hand side evaluated to 1.15243784674 megajoule / kilogram (Allowable error: 0.1%, Actual error: 7.1%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 895046.068456 joule / kilogram but the right hand side evaluated to 0.897474861976 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.13%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1072947.63788 joule / kilogram but the right hand side evaluated to 1.19571380536 megajoule / kilogram (Allowable error: 0.1%, Actual error: 5.6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 596870.993456 joule / kilogram but the right hand side evaluated to 0.615557414011 megajoule / kilogram (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 786926.028536 joule / kilogram but the right hand side evaluated to 0.790365060951 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.22%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.3465569967 meter but the right hand side evaluated to 16.3967794757 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.085409298857229 but the right hand side evaluated to 4.6807905929165345 (Allowable error: 0.1%, Actual error: 58%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.791744900794644 but the right hand side evaluated to 4.680790588367705 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.229132418900267 but the right hand side evaluated to 4.68079059430712 (Allowable error: 0.1%, Actual error: 43%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4249285635 meter but the right hand side evaluated to 18.165987441 meter (Allowable error: 0.1%, Actual error: 1.4%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4249285635 meter but the right hand side evaluated to 18.2854617565 meter (Allowable error: 0.1%, Actual error: 0.76%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3101212431906344 but the right hand side evaluated to 0.19292695632732096 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.24134215237264023 but the right hand side evaluated to 0.17650138831139217 (Allowable error: 0.1%, Actual error: 1.4%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.275042059787921 but the right hand side evaluated to 4.615987439248251 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.453670996964256 but the right hand side evaluated to 4.646345928783959 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2504976.96199 force_pound * meter but the right hand side evaluated to 2454470.94339 force_pound * meter (Allowable error: 0.1%, Actual error: 2.1%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4757972 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116796 meter but the right hand side evaluated to 1.96382947209 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 982256.474784 joule / kilogram but the right hand side evaluated to 1.20546905427 megajoule / kilogram (Allowable error: 0.1%, Actual error: 10%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1151137.21964 joule / kilogram but the right hand side evaluated to 1.88379170556 megajoule / kilogram (Allowable error: 0.1%, Actual error: 25%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4111627137 meter but the right hand side evaluated to 16.4524834421 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.089309646737782 but the right hand side evaluated to 4.73132079850689 (Allowable error: 0.1%, Actual error: 57%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.749131402266716 but the right hand side evaluated to 4.7313207918108695 (Allowable error: 0.1%, Actual error: 51%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.19783341635968 but the right hand side evaluated to 4.7313208008850545 (Allowable error: 0.1%, Actual error: 42%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4749985586 meter but the right hand side evaluated to 18.2223437933 meter (Allowable error: 0.1%, Actual error: 1.4%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4749985586 meter but the right hand side evaluated to 18.3384489934 meter (Allowable error: 0.1%, Actual error: 0.74%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3092784775702393 but the right hand side evaluated to 0.19273737796202528 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2417308179875164 but the right hand side evaluated to 0.17660063303263224 (Allowable error: 0.1%, Actual error: 1.4%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.430221176573312 but the right hand side evaluated to 4.666980446454548 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.495475076392884 but the right hand side evaluated to 4.696716505903449 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2481460.81326 force_pound * meter but the right hand side evaluated to 2426090.46705 force_pound * meter (Allowable error: 0.1%, Actual error: 2.3%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4265323 force_pound but the right hand side evaluated to 32399.9999973 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116724 meter but the right hand side evaluated to 1.83120258472 meter (Allowable error: 0.1%, Actual error: 17%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1203379.25285 joule / kilogram but the right hand side evaluated to 1.66380575713 megajoule / kilogram (Allowable error: 0.1%, Actual error: 17%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4693765328 meter but the right hand side evaluated to 16.6431995085 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 11.047305871339763 but the right hand side evaluated to 4.801805208240624 (Allowable error: 0.1%, Actual error: 57%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.670706476707078 but the right hand side evaluated to 4.80180519047155 (Allowable error: 0.1%, Actual error: 50%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.221372761739048 but the right hand side evaluated to 4.801805213550682 (Allowable error: 0.1%, Actual error: 42%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.6280046731 meter but the right hand side evaluated to 18.344981623 meter (Allowable error: 0.1%, Actual error: 1.5%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.6280046731 meter but the right hand side evaluated to 18.4743856089 meter (Allowable error: 0.1%, Actual error: 0.82%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3268325964867538 but the right hand side evaluated to 0.19660246601770967 (Allowable error: 0.1%, Actual error: 2.8%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2527505607305489 but the right hand side evaluated to 0.17938785978473884 (Allowable error: 0.1%, Actual error: 1.5%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.455616081882331 but the right hand side evaluated to 4.729217744910304 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.548871851608021 but the right hand side evaluated to 4.7625772564597355 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2455567.14873 force_pound * meter but the right hand side evaluated to 2407712.18352 force_pound * meter (Allowable error: 0.1%, Actual error: 2%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.5194988 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116799 meter but the right hand side evaluated to 1.99552129294 meter (Allowable error: 0.1%, Actual error: 9.9%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1227633.95027 joule / kilogram but the right hand side evaluated to 1.72359786474 megajoule / kilogram (Allowable error: 0.1%, Actual error: 18%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 677538.868102 joule / kilogram but the right hand side evaluated to 0.679181882806 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4156361252 meter but the right hand side evaluated to 16.4239734182 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.974970087485737 but the right hand side evaluated to 4.7625548949271295 (Allowable error: 0.1%, Actual error: 57%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.752896877847146 but the right hand side evaluated to 4.762554888461096 (Allowable error: 0.1%, Actual error: 51%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.158718611662756 but the right hand side evaluated to 4.762554896869849 (Allowable error: 0.1%, Actual error: 42%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4488732119 meter but the right hand side evaluated to 18.2046636857 meter (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4488732119 meter but the right hand side evaluated to 18.3176180093 meter (Allowable error: 0.1%, Actual error: 0.71%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3059466178135253 but the right hand side evaluated to 0.1919893382069288 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23934017544917996 but the right hand side evaluated to 0.17598651774707538 (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.504819274720742 but the right hand side evaluated to 4.699783645075703 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.527657124095861 but the right hand side evaluated to 4.728944353131223 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2436785.7555 force_pound * meter but the right hand side evaluated to 2390898.55301 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.474766 force_pound but the right hand side evaluated to 32399.9999989 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116793 meter but the right hand side evaluated to 2.03201037118 meter (Allowable error: 0.1%, Actual error: 8.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1233975.1753 joule / kilogram but the right hand side evaluated to 1.62325875009 megajoule / kilogram (Allowable error: 0.1%, Actual error: 15%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4095779977 meter but the right hand side evaluated to 16.3813524573 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.931049589322477 but the right hand side evaluated to 4.787718614873624 (Allowable error: 0.1%, Actual error: 56%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 9.873362307973842 but the right hand side evaluated to 4.7877186065706505 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.154647489141109 but the right hand side evaluated to 4.787718617011269 (Allowable error: 0.1%, Actual error: 41%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4102724081 meter but the right hand side evaluated to 18.174682543 meter (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4102724081 meter but the right hand side evaluated to 18.2839330388 meter (Allowable error: 0.1%, Actual error: 0.69%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3020986126502745 but the right hand side evaluated to 0.19112015243817296 (Allowable error: 0.1%, Actual error: 2.3%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23685324582841805 but the right hand side evaluated to 0.17534389406193104 (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.536485110930573 but the right hand side evaluated to 4.726722690525297 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.551400752557333 but the right hand side evaluated to 4.755135665323162 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2418323.08088 force_pound * meter but the right hand side evaluated to 2374881.59569 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4976948 force_pound but the right hand side evaluated to 32399.9999985 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.2151011679 meter but the right hand side evaluated to 2.08233880886 meter (Allowable error: 0.1%, Actual error: 6%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1244502.1578 joule / kilogram but the right hand side evaluated to 1.55919668456 megajoule / kilogram (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 664745.775161 joule / kilogram but the right hand side evaluated to 0.667396223732 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.18%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.400049949 meter but the right hand side evaluated to 16.3223962349 meter (Allowable error: 0.1%, Actual error: 13%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.904031786236917 but the right hand side evaluated to 4.789502719298416 (Allowable error: 0.1%, Actual error: 56%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.025948506418324 but the right hand side evaluated to 4.789502710470952 (Allowable error: 0.1%, Actual error: 52%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.145558769824397 but the right hand side evaluated to 4.789502721709762 (Allowable error: 0.1%, Actual error: 41%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3618138158 meter but the right hand side evaluated to 18.1374412497 meter (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3618138158 meter but the right hand side evaluated to 18.241701175 meter (Allowable error: 0.1%, Actual error: 0.65%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.2959632428984156 but the right hand side evaluated to 0.18972227619016538 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2329781340672854 but the right hand side evaluated to 0.17433537586097145 (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.565340890289852 but the right hand side evaluated to 4.731316503962244 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.583806974531507 but the right hand side evaluated to 4.758513653691704 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2405735.06327 force_pound * meter but the right hand side evaluated to 2358168.37085 force_pound * meter (Allowable error: 0.1%, Actual error: 2%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4476315 force_pound but the right hand side evaluated to 32399.9999992 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.2151011681 meter but the right hand side evaluated to 1.97490858687 meter (Allowable error: 0.1%, Actual error: 11%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1245747.42407 joule / kilogram but the right hand side evaluated to 1.35773173764 megajoule / kilogram (Allowable error: 0.1%, Actual error: 4.7%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4441342551 meter but the right hand side evaluated to 16.4749796537 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.933108870618058 but the right hand side evaluated to 4.8317177415246215 (Allowable error: 0.1%, Actual error: 56%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.192140394730561 but the right hand side evaluated to 4.831717724391799 (Allowable error: 0.1%, Actual error: 53%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.195656943420303 but the right hand side evaluated to 4.831717744932532 (Allowable error: 0.1%, Actual error: 41%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4861317628 meter but the right hand side evaluated to 18.2368513416 meter (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4861317628 meter but the right hand side evaluated to 18.3518655919 meter (Allowable error: 0.1%, Actual error: 0.73%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.3102026429341276 but the right hand side evaluated to 0.19294193217855202 (Allowable error: 0.1%, Actual error: 2.5%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2419214696415226 but the right hand side evaluated to 0.17664945013191408 (Allowable error: 0.1%, Actual error: 1.4%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.542128848340953 but the right hand side evaluated to 4.7669782682123705 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.597023261447659 but the right hand side evaluated to 4.79704214391158 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2391780.18296 force_pound * meter but the right hand side evaluated to 2346059.69152 force_pound * meter (Allowable error: 0.1%, Actual error: 1.9%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.4549629 force_pound but the right hand side evaluated to 32399.9999975 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116779 meter but the right hand side evaluated to 2.01208145132 meter (Allowable error: 0.1%, Actual error: 9.2%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1263254.78549 joule / kilogram but the right hand side evaluated to 1.32933821547 megajoule / kilogram (Allowable error: 0.1%, Actual error: 2.8%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 643003.282776 joule / kilogram but the right hand side evaluated to 0.644587887354 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.11%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4391899918 meter but the right hand side evaluated to 16.433303716 meter (Allowable error: 0.1%, Actual error: 12%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.927057749308872 but the right hand side evaluated to 4.827096513659776 (Allowable error: 0.1%, Actual error: 56%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.332846900421936 but the right hand side evaluated to 4.82709645971774 (Allowable error: 0.1%, Actual error: 53%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.188196388869434 but the right hand side evaluated to 4.827096526709544 (Allowable error: 0.1%, Actual error: 41%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.4531719733 meter but the right hand side evaluated to 18.2123809383 meter (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.4531719733 meter but the right hand side evaluated to 18.3237336993 meter (Allowable error: 0.1%, Actual error: 0.7%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.30544742865779373 but the right hand side evaluated to 0.1918757111235145 (Allowable error: 0.1%, Actual error: 2.4%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.2388601883890047 but the right hand side evaluated to 0.17586273874252234 (Allowable error: 0.1%, Actual error: 1.3%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.554288496799318 but the right hand side evaluated to 4.764561457914318 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.6178324601232426 but the right hand side evaluated to 4.793692578920208 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Warning: Constraint [W_{avg}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)*x_{CG}_Mission/CruiseSegment/CruiseP/Aircra... >= 0.225*W_{ht}_Mission/Aircraft/HorizontalTail*x_{CG_{ht}}_Mission/Aircraft/HorizontalTail/HorizontalT...] is not tight because the left hand side evaluated to 2376283.2919 force_pound * meter but the right hand side evaluated to 2334599.85697 force_pound * meter (Allowable error: 0.1%, Actual error: 1.8%) Warning: Constraint [W_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]... >= W_{avg. pass}_Mission/Aircraft/Fuselage*n_{pass}_Mission/Aircraft/Fuselage_(0,) [lbf]...] is not tight because the left hand side evaluated to 32774.458348 force_pound but the right hand side evaluated to 32399.9999986 force_pound (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.0417*S_Mission/Aircraft/Wing/WingNoStruct**-1*\tan(\Lambda)_Mission/Aircraft/Wing/WingNoStruct*b_M... >= \Delta x_{AC_{wing}}_Mission/Aircraft/Wing [m]...] is not tight because the left hand side evaluated to 2.21510116794 meter but the right hand side evaluated to 2.09817158349 meter (Allowable error: 0.1%, Actual error: 5.3%) Warning: Constraint [-C_{p_{fuel}_Mission/Aircraft/Engine/Combustor*T_{t_f}_Mission/Aircraft/Engine/Combustor*f_Mission/A... <= \eta_{B}_Mission/Aircraft/Engine/Combustor*f_Mission/Aircraft/Engine/EnginePerformance/CombustorPerf...] is not tight because the left hand side evaluated to 1283641.19501 joule / kilogram but the right hand side evaluated to 1.28936112023 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.24%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.4146017683 meter but the right hand side evaluated to 16.3183425206 meter (Allowable error: 0.1%, Actual error: 13%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(0, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(0, 0)...] is not tight because the left hand side evaluated to 10.93746433674851 but the right hand side evaluated to 4.82437878982853 (Allowable error: 0.1%, Actual error: 56%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(1, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(1, 0)...] is not tight because the left hand side evaluated to 10.571346237093898 but the right hand side evaluated to 4.824378775447453 (Allowable error: 0.1%, Actual error: 54%) Warning: Constraint [C_{L_{ht}}_Mission/ClimbSegment/ClimbP/AircraftP/HorizontalTailPerformance_(2, 0)*C_{L}_Mission/Clim... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/ClimbSegment/ClimbP/AircraftP_(2, 0)...] is not tight because the left hand side evaluated to 8.19385135123571 but the right hand side evaluated to 4.824378793449321 (Allowable error: 0.1%, Actual error: 41%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) [m]...] is not tight because the left hand side evaluated to 18.3565596046 meter but the right hand side evaluated to 18.1377556347 meter (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [0.25*\Delta x_{AC_{wing}}_Mission/Aircraft/Wing + x_{NP}_Mission/CruiseSegment/CruiseP/AircraftP.1_(... >= x_{AC}_Mission/CruiseSegment/CruiseP. ---------------------------------------------------------------------- Ran 1 test in 112.380s OK Generating XML reports... /AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3565596046 meter but the right hand side evaluated to 18.2401806275 meter (Allowable error: 0.1%, Actual error: 0.63%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 0.2941734366026836 but the right hand side evaluated to 0.18931100822975114 (Allowable error: 0.1%, Actual error: 2.2%) Warning: Constraint [-mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{CG}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0) ... >= SM_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 0.23165615803315465 but the right hand side evaluated to 0.17398914667011375 (Allowable error: 0.1%, Actual error: 1.2%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(0, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(0, 0)...] is not tight because the left hand side evaluated to 7.620071029352279 but the right hand side evaluated to 4.7670198171635985 (Allowable error: 0.1%, Actual error: 37%) Warning: Constraint [C_{L_{ht}}_Mission/CruiseSegment/CruiseP/AircraftP.1/HorizontalTailPerformance.1_(1, 0)*C_{L}_Missio... >= mac_Mission/Aircraft/Wing/WingNoStruct**-1*x_{AC}_Mission/CruiseSegment/CruiseP/AircraftP.1_(1, 0)...] is not tight because the left hand side evaluated to 7.6893941060670805 but the right hand side evaluated to 4.79393946369351 (Allowable error: 0.1%, Actual error: 38%) Solves with these variables bounded: value near lower bound: ClimbDistance_Mission, CruiseAlt_Mission, MaxClimbDistance_Mission, \bar{A}_{fuel, max}_Mission/Aircraft/Wing/WingNoStruct value near upper bound: A_{tri}_Mission/Aircraft/Wing/WingNoStruct, TotalTime_Mission Sweeping took 109 seconds. Cloning into 'solar'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to /tmp/pip-req-build-cVsqzN Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-6pG8LH/wheels/d5/94/ac/b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12 Successfully built gpfit Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to /tmp/pip-req-build-9vPf47 Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2.7.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->gassolar==0.0.0.0) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->gassolar==0.0.0.0) (1.11.0) Building wheels for collected packages: gassolar Running setup.py bdist_wheel for gassolar: started Running setup.py bdist_wheel for gassolar: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-xytxrB/wheels/fe/11/0a/2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar Processing /jenkins/workspace/gplibrary_PR_Models/mosek/solar Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.22.0) Requirement already satisfied: gpfit in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in /jenkins/workspace/gplibrary_PR_Models/mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2.7.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas->solar==0.0.0.0) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas->solar==0.0.0.0) (1.11.0) Building wheels for collected packages: solar Running setup.py bdist_wheel for solar: started Running setup.py bdist_wheel for solar: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-Y3O3Cv/wheels/f6/90/b0/8d5ca9b420ff66bedd24921652ee885c8718a479c0dcec7d2e Successfully built solar Installing collected packages: solar Successfully installed solar-0.0.0.0 Running tests... ---------------------------------------------------------------------- /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) adding test for 'solar/solar.py' adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' Using solver 'mosek' Solving for 9118 variables. Solving took 2.83 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2782 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 867387.0053 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 60.5767138781 ampere but the right hand side evaluated to 573.50220265 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 60.5525990242 ampere but the right hand side evaluated to 573.573550117 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.81%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 60.5172365736 ampere but the right hand side evaluated to 573.639448418 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 60.4636197757 ampere but the right hand side evaluated to 573.740590199 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.64%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 60.382741288 ampere but the right hand side evaluated to 573.915417656 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.47%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 52.7191019462 volt but the right hand side evaluated to 52.2547509424 volt (Allowable error: 0.0001%, Actual error: 0.89%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 52.6335851341 volt but the right hand side evaluated to 52.1977192693 volt (Allowable error: 0.0001%, Actual error: 0.84%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 52.5116747749 volt but the right hand side evaluated to 52.1138994191 volt (Allowable error: 0.0001%, Actual error: 0.76%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 52.3220331613 volt but the right hand side evaluated to 51.9820180648 volt (Allowable error: 0.0001%, Actual error: 0.65%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 52.0211688845 volt but the right hand side evaluated to 51.7700921684 volt (Allowable error: 0.0001%, Actual error: 0.48%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 51.1761770789 ampere but the right hand side evaluated to 488.624313329 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 36.7374875649 volt but the right hand side evaluated to 36.7318130405 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1593765113 ampere but the right hand side evaluated to 488.477326866 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7101651325 volt but the right hand side evaluated to 36.7055494701 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1753622829 ampere but the right hand side evaluated to 488.61716677 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7361657903 volt but the right hand side evaluated to 36.7305412252 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1605703786 ampere but the right hand side evaluated to 488.487772013 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.712106412 volt but the right hand side evaluated to 36.7074155417 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1741322351 ampere but the right hand side evaluated to 488.606397087 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7341667342 volt but the right hand side evaluated to 36.7286190738 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1613463063 ampere but the right hand side evaluated to 488.49456757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.713366745 volt but the right hand side evaluated to 36.7086275393 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1724870196 ampere but the right hand side evaluated to 488.592015453 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7314884536 volt but the right hand side evaluated to 36.7260454658 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1617036131 ampere but the right hand side evaluated to 488.49770625 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7139452382 volt but the right hand side evaluated to 36.7091845126 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1704203139 ampere but the right hand side evaluated to 488.573936571 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7281266666 volt but the right hand side evaluated to 36.7228141557 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 51.1616356352 ampere but the right hand side evaluated to 488.497090762 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 36.7138387563 volt but the right hand side evaluated to 36.7090806819 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1679296669 ampere but the right hand side evaluated to 488.552139935 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7240773101 volt but the right hand side evaluated to 36.7189212892 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1611486684 ampere but the right hand side evaluated to 488.492831233 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7130466915 volt but the right hand side evaluated to 36.7083193696 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1650161594 ampere but the right hand side evaluated to 488.526663937 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7193364341 volt but the right hand side evaluated to 36.7143651295 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1602387382 ampere but the right hand side evaluated to 488.48488025 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7115650738 volt but the right hand side evaluated to 36.7068958609 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1616717032 ampere but the right hand side evaluated to 488.497407578 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7138970302 volt but the right hand side evaluated to 36.7091367809 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1588991298 ampere but the right hand side evaluated to 488.473151418 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.709388485 volt but the right hand side evaluated to 36.7048029805 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1578931666 ampere but the right hand side evaluated to 488.464351441 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7077525301 volt but the right hand side evaluated to 36.7032304902 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1571318803 ampere but the right hand side evaluated to 488.457699672 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7065129349 volt but the right hand side evaluated to 36.7020395328 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1536755511 ampere but the right hand side evaluated to 488.427451058 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7008950918 volt but the right hand side evaluated to 36.6966386599 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [A]... >= 9.55*i0_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.154928807 ampere but the right hand side evaluated to 488.438423802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [V]... >= Kv_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7029310586 volt but the right hand side evaluated to 36.6985963201 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [A]... >= 9.55*i0_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1490156727 ampere but the right hand side evaluated to 488.386694891 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [v_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [V]... >= Kv_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6933165155 volt but the right hand side evaluated to 36.6893545581 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.152286097 ampere but the right hand side evaluated to 488.415295178 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.698635794 volt but the right hand side evaluated to 36.6944668984 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1439036983 ampere but the right hand side evaluated to 488.341970824 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0095%) Warning: Constraint [v_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6850060037 volt but the right hand side evaluated to 36.6813659363 volt (Allowable error: 0.0001%, Actual error: 0.0099%) Warning: Constraint [i_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1492007138 ampere but the right hand side evaluated to 488.388301758 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [v_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6936194012 volt but the right hand side evaluated to 36.6896448406 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1383344748 ampere but the right hand side evaluated to 488.293245795 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) Warning: Constraint [v_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6759531774 volt but the right hand side evaluated to 36.6726636697 volt (Allowable error: 0.0001%, Actual error: 0.009%) Warning: Constraint [i_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1456649362 ampere but the right hand side evaluated to 488.357362609 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0098%) Warning: Constraint [v_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6878721713 volt but the right hand side evaluated to 36.684119863 volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [i_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322987929 ampere but the right hand side evaluated to 488.240426711 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%) Warning: Constraint [v_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661455909 volt but the right hand side evaluated to 36.6632348849 volt (Allowable error: 0.0001%, Actual error: 0.0079%) Warning: Constraint [i_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1416734757 ampere but the right hand side evaluated to 488.322439217 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0091%) Warning: Constraint [v_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6813840482 volt but the right hand side evaluated to 36.6778828409 volt (Allowable error: 0.0001%, Actual error: 0.0095%) Warning: Constraint [i_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1257892737 ampere but the right hand side evaluated to 488.183454862 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0065%) Warning: Constraint [v_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6555704064 volt but the right hand side evaluated to 36.653067643 volt (Allowable error: 0.0001%, Actual error: 0.0068%) Warning: Constraint [i_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1372185679 ampere but the right hand side evaluated to 488.283459165 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0084%) Warning: Constraint [v_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6741434729 volt but the right hand side evaluated to 36.6709223357 volt (Allowable error: 0.0001%, Actual error: 0.0088%) Warning: Constraint [i_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1187974681 ampere but the right hand side evaluated to 488.122259522 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0054%) Warning: Constraint [v_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6442135106 volt but the right hand side evaluated to 36.6421485984 volt (Allowable error: 0.0001%, Actual error: 0.0056%) Warning: Constraint [i_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322923704 ampere but the right hand side evaluated to 488.240353768 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%) Warning: Constraint [v_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661379023 volt but the right hand side evaluated to 36.6632262758 volt (Allowable error: 0.0001%, Actual error: 0.0079%) Warning: Constraint [i_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1113204161 ampere but the right hand side evaluated to 488.056861865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0042%) Warning: Constraint [v_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6320611515 volt but the right hand side evaluated to 36.6304678418 volt (Allowable error: 0.0001%, Actual error: 0.0043%) Warning: Constraint [i_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1268883963 ampere but the right hand side evaluated to 488.193080771 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0067%) Warning: Constraint [v_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6573541028 volt but the right hand side evaluated to 36.6547829533 volt (Allowable error: 0.0001%, Actual error: 0.007%) Warning: Constraint [i_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.103334686 ampere but the right hand side evaluated to 487.986966523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [v_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6190933328 volt but the right hand side evaluated to 36.6179997286 volt (Allowable error: 0.0001%, Actual error: 0.003%) Warning: Constraint [i_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1209900914 ampere but the right hand side evaluated to 488.14144535 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0057%) Warning: Constraint [v_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6477752562 volt but the right hand side evaluated to 36.6455726465 volt (Allowable error: 0.0001%, Actual error: 0.006%) Warning: Constraint [i_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.094834742 ampere but the right hand side evaluated to 487.912565101 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0015%) Warning: Constraint [v_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6052934087 volt but the right hand side evaluated to 36.6047310684 volt (Allowable error: 0.0001%, Actual error: 0.0015%) Warning: Constraint [i_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1145971449 ampere but the right hand side evaluated to 488.085516152 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0047%) Warning: Constraint [v_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6373870858 volt but the right hand side evaluated to 36.6355866842 volt (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound i/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/gassolar/environment/solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) s 0.0500 Using solver 'mosek' Solving for 9118 variables. Solving took 2.1 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2362 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 996075.2388 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4799094159 ampere but the right hand side evaluated to 615.821326952 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4269408529 ampere but the right hand side evaluated to 615.857534962 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.3537417222 ampere but the right hand side evaluated to 615.884626715 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.2456816235 ampere but the right hand side evaluated to 615.958694347 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.088823125 ampere but the right hand side evaluated to 616.178883569 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.6838766903 volt but the right hand side evaluated to 60.7352062815 volt (Allowable error: 0.0001%, Actual error: 1.6%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.5684241079 volt but the right hand side evaluated to 60.6742768192 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.4033727713 volt but the right hand side evaluated to 60.5823029137 volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.1440198666 volt but the right hand side evaluated to 60.4342146467 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 60.7247881215 volt but the right hand side evaluated to 60.1876338227 volt (Allowable error: 0.0001%, Actual error: 0.89%) Warning: Constraint [i_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [A]... >= 9.55*i0_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6303100545 ampere but the right hand side evaluated to 530.635190047 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [V]... >= Kv_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6648172956 volt but the right hand side evaluated to 43.6139158349 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [A]... >= 9.55*i0_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6196605331 ampere but the right hand side evaluated to 530.541236151 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [V]... >= Kv_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6463708457 volt but the right hand side evaluated to 43.5961417227 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [A]... >= 9.55*i0_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5957636688 ampere but the right hand side evaluated to 530.330931472 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [V]... >= Kv_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6045418941 volt but the right hand side evaluated to 43.5558653394 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [A]... >= 9.55*i0_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5878440231 ampere but the right hand side evaluated to 530.263276481 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [V]... >= Kv_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.590780003 volt but the right hand side evaluated to 43.5427920757 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [A]... >= 9.55*i0_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5610277283 ampere but the right hand side evaluated to 530.027651447 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [V]... >= Kv_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5438807304 volt but the right hand side evaluated to 43.4976645311 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [A]... >= 9.55*i0_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5555830194 ampere but the right hand side evaluated to 529.98108812 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [V]... >= Kv_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5344970189 volt but the right hand side evaluated to 43.4887493181 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [A]... >= 9.55*i0_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5259608011 ampere but the right hand side evaluated to 529.722783208 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.096%) Warning: Constraint [v_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [V]... >= Kv_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4826878182 volt but the right hand side evaluated to 43.4390632043 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [A]... >= 9.55*i0_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5229259664 ampere but the right hand side evaluated to 529.695586633 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.096%) Warning: Constraint [v_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [V]... >= Kv_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4775184038 volt but the right hand side evaluated to 43.4340485586 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [A]... >= 9.55*i0_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4903788581 ampere but the right hand side evaluated to 529.411876726 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [v_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [V]... >= Kv_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4205963539 volt but the right hand side evaluated to 43.3794647812 volt (Allowable error: 0.0001%, Actual error: 0.095%) Warning: Constraint [i_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [A]... >= 9.55*i0_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4899305274 ampere but the right hand side evaluated to 529.407817905 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [v_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [V]... >= Kv_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4198391055 volt but the right hand side evaluated to 43.378726852 volt (Allowable error: 0.0001%, Actual error: 0.095%) Warning: Constraint [i_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [A]... >= 9.55*i0_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4544026066 ampere but the right hand side evaluated to 529.097898426 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%) Warning: Constraint [v_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [V]... >= Kv_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3577733942 volt but the right hand side evaluated to 43.3191909295 volt (Allowable error: 0.0001%, Actual error: 0.089%) Warning: Constraint [i_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [A]... >= 9.55*i0_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4563468598 ampere but the right hand side evaluated to 529.113898151 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%) Warning: Constraint [v_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [V]... >= Kv_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.361350614 volt but the right hand side evaluated to 43.3225478549 volt (Allowable error: 0.0001%, Actual error: 0.09%) Warning: Constraint [i_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [A]... >= 9.55*i0_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4179070625 ampere but the right hand side evaluated to 528.77897852 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [v_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [V]... >= Kv_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2941488702 volt but the right hand side evaluated to 43.2581138251 volt (Allowable error: 0.0001%, Actual error: 0.083%) Warning: Constraint [i_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [A]... >= 9.55*i0_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4224315845 ampere but the right hand side evaluated to 528.818089866 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [v_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [V]... >= Kv_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3021151085 volt but the right hand side evaluated to 43.26572807 volt (Allowable error: 0.0001%, Actual error: 0.084%) Warning: Constraint [i_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [A]... >= 9.55*i0_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3809363615 ampere but the right hand side evaluated to 528.455960433 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.074%) Warning: Constraint [v_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [V]... >= Kv_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2297072076 volt but the right hand side evaluated to 43.1962537345 volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [i_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [A]... >= 9.55*i0_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3879091315 ampere but the right hand side evaluated to 528.516101168 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [V]... >= Kv_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2420129723 volt but the right hand side evaluated to 43.2080063255 volt (Allowable error: 0.0001%, Actual error: 0.079%) Warning: Constraint [i_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [A]... >= 9.55*i0_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3434187786 ampere but the right hand side evaluated to 528.127894374 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [v_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [V]... >= Kv_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1644036157 volt but the right hand side evaluated to 43.1335432029 volt (Allowable error: 0.0001%, Actual error: 0.072%) Warning: Constraint [i_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [A]... >= 9.55*i0_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3528929777 ampere but the right hand side evaluated to 528.209906647 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) Warning: Constraint [v_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [V]... >= Kv_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.181056378 volt but the right hand side evaluated to 43.1494705658 volt (Allowable error: 0.0001%, Actual error: 0.073%) Warning: Constraint [i_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [A]... >= 9.55*i0_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3053498752 ampere but the right hand side evaluated to 527.794856279 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [V]... >= Kv_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0982043851 volt but the right hand side evaluated to 43.0699584744 volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [i_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [A]... >= 9.55*i0_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3173959025 ampere but the right hand side evaluated to 527.899861509 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.065%) Warning: Constraint [v_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [V]... >= Kv_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1192211978 volt but the right hand side evaluated to 43.0901163312 volt (Allowable error: 0.0001%, Actual error: 0.068%) Warning: Constraint [i_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [A]... >= 9.55*i0_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2667585093 ampere but the right hand side evaluated to 527.457450562 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.057%) Warning: Constraint [v_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [V]... >= Kv_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0310835967 volt but the right hand side evaluated to 43.0055014246 volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [i_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [A]... >= 9.55*i0_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2813120089 ampere but the right hand side evaluated to 527.584423468 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [v_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [V]... >= Kv_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0564429155 volt but the right hand side evaluated to 43.0298338101 volt (Allowable error: 0.0001%, Actual error: 0.062%) Warning: Constraint [i_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [A]... >= 9.55*i0_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2276082214 ampere but the right hand side evaluated to 527.115260236 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [V]... >= Kv_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9629958701 volt but the right hand side evaluated to 42.9401206391 volt (Allowable error: 0.0001%, Actual error: 0.053%) Warning: Constraint [i_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [A]... >= 9.55*i0_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2446584253 ampere but the right hand side evaluated to 527.264032777 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [v_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [V]... >= Kv_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9926969664 volt but the right hand side evaluated to 42.9686218099 volt (Allowable error: 0.0001%, Actual error: 0.056%) Warning: Constraint [i_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [A]... >= 9.55*i0_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1878188477 ampere but the right hand side evaluated to 526.767196792 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [v_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [V]... >= Kv_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8938839987 volt but the right hand side evaluated to 42.8737313363 volt (Allowable error: 0.0001%, Actual error: 0.047%) Warning: Constraint [i_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [A]... >= 9.55*i0_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2073791949 ampere but the right hand side evaluated to 526.937964065 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [v_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [V]... >= Kv_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9279333033 volt but the right hand side evaluated to 42.9064139177 volt (Allowable error: 0.0001%, Actual error: 0.05%) Warning: Constraint [i_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [A]... >= 9.55*i0_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1473783892 ampere but the right hand side evaluated to 526.413344983 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [v_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [V]... >= Kv_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8237241376 volt but the right hand side evaluated to 42.8063264187 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [A]... >= 9.55*i0_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1694858566 ampere but the right hand side evaluated to 526.606581069 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.042%) Warning: Constraint [v_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [V]... >= Kv_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8621225845 volt but the right hand side evaluated to 42.8432021419 volt (Allowable error: 0.0001%, Actual error: 0.044%) Warning: Constraint [i_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [A]... >= 9.55*i0_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1063077258 ampere but the right hand side evaluated to 526.05410498 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.033%) Warning: Constraint [v_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [V]... >= Kv_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7524642558 volt but the right hand side evaluated to 42.7378706733 volt (Allowable error: 0.0001%, Actual error: 0.034%) Warning: Constraint [i_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [A]... >= 9.55*i0_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1309432934 ampere but the right hand side evaluated to 526.269508859 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.037%) Warning: Constraint [v_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [V]... >= Kv_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7952189067 volt but the right hand side evaluated to 42.778937035 volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [i_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [A]... >= 9.55*i0_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0645461099 ampere but the right hand side evaluated to 525.688760647 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [V]... >= Kv_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6800552972 volt but the right hand side evaluated to 42.6683033033 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [A]... >= 9.55*i0_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.091723572 ampere but the right hand side evaluated to 525.926494875 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.031%) Warning: Constraint [v_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [V]... >= Kv_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7271769282 volt but the right hand side evaluated to 42.7135742624 volt (Allowable error: 0.0001%, Actual error: 0.032%) Warning: Constraint [i_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [A]... >= 9.55*i0_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0220666538 ampere but the right hand side evaluated to 525.317097433 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.02%) Warning: Constraint [v_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [V]... >= Kv_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.606448978 volt but the right hand side evaluated to 42.5975793774 volt (Allowable error: 0.0001%, Actual error: 0.021%) Warning: Constraint [i_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [A]... >= 9.55*i0_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0517832313 ampere but the right hand side evaluated to 525.577048469 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.024%) Warning: Constraint [v_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [V]... >= Kv_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6579448219 volt but the right hand side evaluated to 42.6470553974 volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [i_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [A]... >= 9.55*i0_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9788256871 ampere but the right hand side evaluated to 524.938640627 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [V]... >= Kv_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5315895601 volt but the right hand side evaluated to 42.5256380513 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [A]... >= 9.55*i0_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0110964967 ampere but the right hand side evaluated to 525.220972102 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.018%) Warning: Constraint [v_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [V]... >= Kv_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5874745244 volt but the right hand side evaluated to 42.5793362813 volt (Allowable error: 0.0001%, Actual error: 0.019%) Warning: Constraint [i_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [A]... >= 9.55*i0_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9347886725 ampere but the right hand side evaluated to 524.553073363 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0068%) Warning: Constraint [v_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [V]... >= Kv_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.4554224477 volt but the right hand side evaluated to 42.4524255873 volt (Allowable error: 0.0001%, Actual error: 0.0071%) Warning: Constraint [i_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [A]... >= 9.55*i0_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9696415114 ampere but the right hand side evaluated to 524.858145514 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [V]... >= Kv_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5157166019 volt but the right hand side evaluated to 42.51037473 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500 Using solver 'mosek' Solving for 9118 variables. Solving took 1.66 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1906 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 1169782.8943 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/TailAero.165_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/TailAe could cause inaccurate result because it is above upper bound. Solution is 1085313.8783 but bound is 1000000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500 Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.516849901 ampere but the right hand side evaluated to 674.454725588 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.4534913807 ampere but the right hand side evaluated to 674.321289992 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.36552124 ampere but the right hand side evaluated to 674.11034633 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.2344809697 ampere but the right hand side evaluated to 673.812557079 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.95%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.04028701 ampere but the right hand side evaluated to 673.430744619 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.8209546682 volt but the right hand side evaluated to 71.9033737911 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.720190811 volt but the right hand side evaluated to 71.8534184136 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.5730825537 volt but the right hand side evaluated to 71.7741989216 volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.3412452394 volt but the right hand side evaluated to 71.6453767545 volt (Allowable error: 0.0001%, Actual error: 0.97%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.9657525744 volt but the right hand side evaluated to 71.4291750064 volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [A]... >= 9.55*i0_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6891675551 ampere but the right hand side evaluated to 578.394601057 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [V]... >= Kv_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1934112889 volt but the right hand side evaluated to 52.0867037906 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [A]... >= 9.55*i0_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6859574783 ampere but the right hand side evaluated to 578.363158732 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [V]... >= Kv_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1879222725 volt but the right hand side evaluated to 52.0811468255 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [A]... >= 9.55*i0_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6183905055 ampere but the right hand side evaluated to 577.777231104 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [V]... >= Kv_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0615517253 volt but the right hand side evaluated to 51.9604184304 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [A]... >= 9.55*i0_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6170141714 ampere but the right hand side evaluated to 577.759319582 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [V]... >= Kv_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0598404361 volt but the right hand side evaluated to 51.9582651148 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [A]... >= 9.55*i0_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5476972409 ampere but the right hand side evaluated to 577.163280074 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [V]... >= Kv_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9295200825 volt but the right hand side evaluated to 51.8341919708 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [A]... >= 9.55*i0_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.548230469 ampere but the right hand side evaluated to 577.160359929 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [V]... >= Kv_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9316143757 volt but the right hand side evaluated to 51.8355397615 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [A]... >= 9.55*i0_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4762140002 ampere but the right hand side evaluated to 576.537928642 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [V]... >= Kv_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.7967371597 volt but the right hand side evaluated to 51.7068436825 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [A]... >= 9.55*i0_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4789746224 ampere but the right hand side evaluated to 576.555629392 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [V]... >= Kv_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.8028099723 volt but the right hand side evaluated to 51.7121072677 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [A]... >= 9.55*i0_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4040217488 ampere but the right hand side evaluated to 575.902958884 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [V]... >= Kv_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6632135633 volt but the right hand side evaluated to 51.5784787765 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [A]... >= 9.55*i0_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4093901872 ampere but the right hand side evaluated to 575.947948979 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [V]... >= Kv_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6734696615 volt but the right hand side evaluated to 51.5881447759 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [A]... >= 9.55*i0_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3322764096 ampere but the right hand side evaluated to 575.27868648 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [V]... >= Kv_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5295875025 volt but the right hand side evaluated to 51.4505950205 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [A]... >= 9.55*i0_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3393039641 ampere but the right hand side evaluated to 575.334660432 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [V]... >= Kv_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5434447526 volt but the right hand side evaluated to 51.4634105044 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [A]... >= 9.55*i0_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2597676648 ampere but the right hand side evaluated to 574.644540392 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [V]... >= Kv_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.3950902524 volt but the right hand side evaluated to 51.321588263 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [A]... >= 9.55*i0_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2690875028 ampere but the right hand side evaluated to 574.72250688 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [V]... >= Kv_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.4129058694 volt but the right hand side evaluated to 51.3383707064 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [A]... >= 9.55*i0_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1865901805 ampere but the right hand side evaluated to 574.002529587 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [V]... >= Kv_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2597330842 volt but the right hand side evaluated to 51.1915725293 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [A]... >= 9.55*i0_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1983276255 ampere but the right hand side evaluated to 574.104697293 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [V]... >= Kv_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2815611479 volt but the right hand side evaluated to 51.2124698672 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [A]... >= 9.55*i0_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1132850692 ampere but the right hand side evaluated to 573.362314695 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [V]... >= Kv_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.1237757962 volt but the right hand side evaluated to 51.0612225024 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [A]... >= 9.55*i0_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.1268533147 ampere but the right hand side evaluated to 573.478647865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [V]... >= Kv_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.1492654085 volt but the right hand side evaluated to 51.0854751152 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [A]... >= 9.55*i0_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0393282196 ampere but the right hand side evaluated to 572.715244999 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [V]... >= Kv_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 50.9868645595 volt but the right hand side evaluated to 50.9298473266 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [A]... >= 9.55*i0_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0551313861 ampere but the right hand side evaluated to 572.852726265 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [V]... >= Kv_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.0162338548 volt but the right hand side evaluated to 50.9579623419 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [A]... >= 9.55*i0_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.964800155 ampere but the right hand side evaluated to 572.063077027 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [V]... >= Kv_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8489923359 volt but the right hand side evaluated to 50.797530919 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [A]... >= 9.55*i0_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9826335702 ampere but the right hand side evaluated to 572.218228306 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8821153141 volt but the right hand side evaluated to 50.829242541 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8896223267 ampere but the right hand side evaluated to 571.404845931 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [V]... >= Kv_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7100604464 volt but the right hand side evaluated to 50.6641545814 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9096688675 ampere but the right hand side evaluated to 571.580812986 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.09%) Warning: Constraint [v_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [V]... >= Kv_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.747029002 volt but the right hand side evaluated to 50.6996841923 volt (Allowable error: 0.0001%, Actual error: 0.093%) Warning: Constraint [i_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [A]... >= 9.55*i0_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8136229022 ampere but the right hand side evaluated to 570.738012198 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [v_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [V]... >= Kv_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.5699194508 volt but the right hand side evaluated to 50.5294861329 volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [i_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [A]... >= 9.55*i0_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8359692188 ampere but the right hand side evaluated to 570.936271541 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [v_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [V]... >= Kv_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.6107710254 volt but the right hand side evaluated to 50.5689312719 volt (Allowable error: 0.0001%, Actual error: 0.083%) Warning: Constraint [i_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [A]... >= 9.55*i0_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7374275173 ampere but the right hand side evaluated to 570.073623032 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [v_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [V]... >= Kv_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.428845873 volt but the right hand side evaluated to 50.3942673954 volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [i_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [A]... >= 9.55*i0_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7615480468 ampere but the right hand side evaluated to 570.285222641 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [v_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [V]... >= Kv_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.4732923448 volt but the right hand side evaluated to 50.436979582 volt (Allowable error: 0.0001%, Actual error: 0.072%) Warning: Constraint [i_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [A]... >= 9.55*i0_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6602284637 ampere but the right hand side evaluated to 569.398329224 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [v_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [V]... >= Kv_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.286343927 volt but the right hand side evaluated to 50.2574846396 volt (Allowable error: 0.0001%, Actual error: 0.057%) Warning: Constraint [i_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [A]... >= 9.55*i0_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.686301657 ampere but the right hand side evaluated to 569.626300685 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [v_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [V]... >= Kv_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.3344787357 volt but the right hand side evaluated to 50.3036801594 volt (Allowable error: 0.0001%, Actual error: 0.061%) Warning: Constraint [i_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [A]... >= 9.55*i0_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5818382925 ampere but the right hand side evaluated to 568.709392522 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [v_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [V]... >= Kv_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1422572354 volt but the right hand side evaluated to 50.1188949301 volt (Allowable error: 0.0001%, Actual error: 0.047%) Warning: Constraint [i_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [A]... >= 9.55*i0_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6102102746 ampere but the right hand side evaluated to 568.95958329 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) Warning: Constraint [v_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [V]... >= Kv_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1942593042 volt but the right hand side evaluated to 50.1689862624 volt (Allowable error: 0.0001%, Actual error: 0.05%) Warning: Constraint [i_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [A]... >= 9.55*i0_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5031049583 ampere but the right hand side evaluated to 568.021622378 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.034%) Warning: Constraint [v_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [V]... >= Kv_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9969613809 volt but the right hand side evaluated to 49.9794876681 volt (Allowable error: 0.0001%, Actual error: 0.035%) Warning: Constraint [i_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [A]... >= 9.55*i0_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5333088076 ampere but the right hand side evaluated to 568.286086137 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [V]... >= Kv_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.0525886386 volt but the right hand side evaluated to 50.03291451 volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [i_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [A]... >= 9.55*i0_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4232594944 ampere but the right hand side evaluated to 567.322439102 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.023%) Warning: Constraint [v_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [V]... >= Kv_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.8499894193 volt but the right hand side evaluated to 49.8383161992 volt (Allowable error: 0.0001%, Actual error: 0.023%) Warning: Constraint [i_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [A]... >= 9.55*i0_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4555333888 ampere but the right hand side evaluated to 567.605160492 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9093663 volt but the right hand side evaluated to 49.8953603145 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [A]... >= 9.55*i0_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3423912983 ampere but the right hand side evaluated to 566.613823251 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [V]... >= Kv_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7013168616 volt but the right hand side evaluated to 49.6954586905 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [A]... >= 9.55*i0_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3767329571 ampere but the right hand side evaluated to 566.91470593 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.016%) Warning: Constraint [v_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [V]... >= Kv_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7644456651 volt but the right hand side evaluated to 49.7561164378 volt (Allowable error: 0.0001%, Actual error: 0.017%) Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500 Warning: Constraint [i_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [A]... >= 9.55*i0_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.2969058261 ampere but the right hand side evaluated to 566.215203076 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.005%) Warning: Constraint [v_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [V]... >= Kv_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.6177491495 volt but the right hand side evaluated to 49.6151501088 volt (Allowable error: 0.0001%, Actual error: 0.0052%) Using solver 'mosek' Solving for 4738 variables. Solving took 1.26 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1350804.6897 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.246_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1008642.4806 but bound is 1000000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.247_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1292032.3843 but bound is 1000000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4850350238 ampere but the right hand side evaluated to 734.385435807 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4268952323 ampere but the right hand side evaluated to 734.137686981 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.3444196382 ampere but the right hand side evaluated to 733.758427731 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.2198355874 ampere but the right hand side evaluated to 733.184352769 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.0308280737 ampere but the right hand side evaluated to 732.3235153 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 85.0571755001 volt but the right hand side evaluated to 84.4091401145 volt (Allowable error: 0.0001%, Actual error: 0.77%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.9749627193 volt but the right hand side evaluated to 84.3626533554 volt (Allowable error: 0.0001%, Actual error: 0.73%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.8508247376 volt but the right hand side evaluated to 84.2860526741 volt (Allowable error: 0.0001%, Actual error: 0.67%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.6551051027 volt but the right hand side evaluated to 84.1621011297 volt (Allowable error: 0.0001%, Actual error: 0.59%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.3396081983 volt but the right hand side evaluated to 83.9568525684 volt (Allowable error: 0.0001%, Actual error: 0.46%) Warning: Constraint [i_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [A]... >= 9.55*i0_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6950623605 ampere but the right hand side evaluated to 625.910782851 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [V]... >= Kv_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.2753343689 volt but the right hand side evaluated to 61.1311457089 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [A]... >= 9.55*i0_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6042102871 ampere but the right hand side evaluated to 625.12119117 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [V]... >= Kv_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.097423962 volt but the right hand side evaluated to 60.9612686885 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [A]... >= 9.55*i0_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.5127067043 ampere but the right hand side evaluated to 624.32018677 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [V]... >= Kv_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.9187739886 volt but the right hand side evaluated to 60.7901124939 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [A]... >= 9.55*i0_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.4210265459 ampere but the right hand side evaluated to 623.517507216 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [V]... >= Kv_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.7398459528 volt but the right hand side evaluated to 60.6186609409 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [A]... >= 9.55*i0_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.3291328362 ampere but the right hand side evaluated to 622.71293019 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [V]... >= Kv_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.5605431419 volt but the right hand side evaluated to 60.4468303616 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [A]... >= 9.55*i0_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.2367398876 ampere but the right hand side evaluated to 621.901612414 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [V]... >= Kv_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.3805437668 volt but the right hand side evaluated to 60.2740876681 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [A]... >= 9.55*i0_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.1444900239 ampere but the right hand side evaluated to 621.096169187 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [V]... >= Kv_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.2004046181 volt but the right hand side evaluated to 60.1016366776 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [A]... >= 9.55*i0_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.0516185812 ampere but the right hand side evaluated to 620.282763453 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [V]... >= Kv_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.0193502633 volt but the right hand side evaluated to 59.9280492878 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [A]... >= 9.55*i0_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.9582662528 ampere but the right hand side evaluated to 619.464639921 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [V]... >= Kv_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.8374717073 volt but the right hand side evaluated to 59.7536062419 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [A]... >= 9.55*i0_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.8637890029 ampere but the right hand side evaluated to 618.629888976 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [V]... >= Kv_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.6540396769 volt but the right hand side evaluated to 59.5770057956 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [A]... >= 9.55*i0_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.7700779093 ampere but the right hand side evaluated to 617.815478832 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [V]... >= Kv_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.4709420728 volt but the right hand side evaluated to 59.4020147242 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [A]... >= 9.55*i0_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.6750113509 ampere but the right hand side evaluated to 616.981311697 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [V]... >= Kv_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.2859761279 volt but the right hand side evaluated to 59.2244586771 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [A]... >= 9.55*i0_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.5796244927 ampere but the right hand side evaluated to 616.14775717 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [V]... >= Kv_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.1001161502 volt but the right hand side evaluated to 59.0463523396 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [A]... >= 9.55*i0_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.4834166573 ampere but the right hand side evaluated to 615.305875297 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [V]... >= Kv_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.912808811 volt but the right hand side evaluated to 58.8667294663 volt (Allowable error: 0.0001%, Actual error: 0.078%) Warning: Constraint [i_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [A]... >= 9.55*i0_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.3862721272 ampere but the right hand side evaluated to 614.454268429 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [V]... >= Kv_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.7239171238 volt but the right hand side evaluated to 58.6854240245 volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [i_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [A]... >= 9.55*i0_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.2882277913 ampere but the right hand side evaluated to 613.594248829 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [V]... >= Kv_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.5334083883 volt but the right hand side evaluated to 58.5024979672 volt (Allowable error: 0.0001%, Actual error: 0.053%) Warning: Constraint [i_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [A]... >= 9.55*i0_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.1893566225 ampere but the right hand side evaluated to 612.727782775 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [V]... >= Kv_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140**-1*omega_Mission.3/F...]. is not tight because the left hand side evaluated to 58.3412714204 volt but the right hand side evaluated to 58.3180647306 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [A]... >= 9.55*i0_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.0894250062 ampere but the right hand side evaluated to 611.851264256 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [V]... >= Kv_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.1472427727 volt but the right hand side evaluated to 58.1317245864 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [A]... >= 9.55*i0_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 63.9884466679 ampere but the right hand side evaluated to 610.965622708 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [V]... >= Kv_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 57.9512573663 volt but the right hand side evaluated to 57.943490413 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Using solver 'mosek' Solving for 9118 variables. Solving took 2.02 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.2782 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 867387.0043 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 60.5767140851 ampere but the right hand side evaluated to 573.502206949 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 60.5525991799 ampere but the right hand side evaluated to 573.573553256 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.81%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 60.5172366648 ampere but the right hand side evaluated to 573.639450147 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 60.4636197801 ampere but the right hand side evaluated to 573.740590117 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.64%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 60.3827411939 ampere but the right hand side evaluated to 573.915415662 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.47%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 52.7191013201 volt but the right hand side evaluated to 52.2547505355 volt (Allowable error: 0.0001%, Actual error: 0.89%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 52.6335846797 volt but the right hand side evaluated to 52.1977189707 volt (Allowable error: 0.0001%, Actual error: 0.84%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 52.5116745268 volt but the right hand side evaluated to 52.1138992516 volt (Allowable error: 0.0001%, Actual error: 0.76%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 52.3220331732 volt but the right hand side evaluated to 51.9820180648 volt (Allowable error: 0.0001%, Actual error: 0.65%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 52.0211691628 volt but the right hand side evaluated to 51.770092344 volt (Allowable error: 0.0001%, Actual error: 0.48%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 51.1761770026 ampere but the right hand side evaluated to 488.624312531 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 36.7374875084 volt but the right hand side evaluated to 36.7318129784 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1593764452 ampere but the right hand side evaluated to 488.477326201 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7101650739 volt but the right hand side evaluated to 36.7055494087 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1753622077 ampere but the right hand side evaluated to 488.617165988 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7361657338 volt but the right hand side evaluated to 36.7305411636 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1605703119 ampere but the right hand side evaluated to 488.487771339 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7121063536 volt but the right hand side evaluated to 36.7074154802 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1741321613 ampere but the right hand side evaluated to 488.606396324 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7341666776 volt but the right hand side evaluated to 36.7286190124 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1613462387 ampere but the right hand side evaluated to 488.494566885 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7133666867 volt but the right hand side evaluated to 36.7086274777 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1724869455 ampere but the right hand side evaluated to 488.592014686 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7314883968 volt but the right hand side evaluated to 36.7260454043 volt (Allowable error: 0.0001%, Actual error: 0.015%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1617035448 ampere but the right hand side evaluated to 488.497705556 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.71394518 volt but the right hand side evaluated to 36.7091844509 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 51.1704202407 ampere but the right hand side evaluated to 488.573935816 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 36.7281266097 volt but the right hand side evaluated to 36.7228140943 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 51.1616355677 ampere but the right hand side evaluated to 488.49709008 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 36.7138386981 volt but the right hand side evaluated to 36.7090806206 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1679295957 ampere but the right hand side evaluated to 488.552139206 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7240772528 volt but the right hand side evaluated to 36.718921228 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.161148601 ampere but the right hand side evaluated to 488.492830552 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7130466332 volt but the right hand side evaluated to 36.7083193084 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1650160885 ampere but the right hand side evaluated to 488.526663212 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7193363765 volt but the right hand side evaluated to 36.714365068 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1602386706 ampere but the right hand side evaluated to 488.484879567 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7115650156 volt but the right hand side evaluated to 36.7068957996 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.161671634 ampere but the right hand side evaluated to 488.497406873 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7138969723 volt but the right hand side evaluated to 36.7091367194 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1588990631 ampere but the right hand side evaluated to 488.473150747 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7093884267 volt but the right hand side evaluated to 36.7048029193 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1578930993 ampere but the right hand side evaluated to 488.464350762 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7077524717 volt but the right hand side evaluated to 36.7032304288 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.157131814 ampere but the right hand side evaluated to 488.457699005 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.7065128764 volt but the right hand side evaluated to 36.7020394717 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1536754862 ampere but the right hand side evaluated to 488.42745041 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.700895033 volt but the right hand side evaluated to 36.6966385986 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [A]... >= 9.55*i0_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1549287414 ampere but the right hand side evaluated to 488.438423145 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20 [V]... >= Kv_Mission/FlightSegment.19/AircraftPerf.19/AircraftDrag.20/MotorPerf.20**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.702931 volt but the right hand side evaluated to 36.6985962591 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [A]... >= 9.55*i0_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.149015609 ampere but the right hand side evaluated to 488.386694254 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [v_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21 [V]... >= Kv_Mission/FlightSegment.20/AircraftPerf.20/AircraftDrag.21/MotorPerf.21**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.693316456 volt but the right hand side evaluated to 36.6893544963 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1522860278 ampere but the right hand side evaluated to 488.415294471 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission/FlightSegment.21/AircraftPerf.21/AircraftDrag.22/MotorPerf.22**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6986357354 volt but the right hand side evaluated to 36.6944668361 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1439036373 ampere but the right hand side evaluated to 488.341970222 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0095%) Warning: Constraint [v_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission/FlightSegment.22/AircraftPerf.22/AircraftDrag.23/MotorPerf.23**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6850059436 volt but the right hand side evaluated to 36.6813658746 volt (Allowable error: 0.0001%, Actual error: 0.0099%) Warning: Constraint [i_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1492006504 ampere but the right hand side evaluated to 488.38830113 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [v_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission/FlightSegment.23/AircraftPerf.23/AircraftDrag.24/MotorPerf.24**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6936193421 volt but the right hand side evaluated to 36.6896447797 volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [i_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1383344148 ampere but the right hand side evaluated to 488.293245201 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) Warning: Constraint [v_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission/FlightSegment.24/AircraftPerf.24/AircraftDrag.25/MotorPerf.25**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6759531166 volt but the right hand side evaluated to 36.6726636071 volt (Allowable error: 0.0001%, Actual error: 0.009%) Warning: Constraint [i_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1456648687 ampere but the right hand side evaluated to 488.357361922 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0098%) Warning: Constraint [v_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission/FlightSegment.25/AircraftPerf.25/AircraftDrag.26/MotorPerf.26**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6878721121 volt but the right hand side evaluated to 36.6841198005 volt (Allowable error: 0.0001%, Actual error: 0.01%) Warning: Constraint [i_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322987352 ampere but the right hand side evaluated to 488.240426144 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%) Warning: Constraint [v_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission/FlightSegment.26/AircraftPerf.26/AircraftDrag.27/MotorPerf.27**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661455293 volt but the right hand side evaluated to 36.663234822 volt (Allowable error: 0.0001%, Actual error: 0.0079%) Warning: Constraint [i_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1416734091 ampere but the right hand side evaluated to 488.322438541 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0091%) Warning: Constraint [v_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission/FlightSegment.27/AircraftPerf.27/AircraftDrag.28/MotorPerf.28**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6813839886 volt but the right hand side evaluated to 36.6778827782 volt (Allowable error: 0.0001%, Actual error: 0.0095%) Warning: Constraint [i_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1257892059 ampere but the right hand side evaluated to 488.183454152 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0065%) Warning: Constraint [v_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission/FlightSegment.28/AircraftPerf.28/AircraftDrag.29/MotorPerf.29**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6555703447 volt but the right hand side evaluated to 36.6530675762 volt (Allowable error: 0.0001%, Actual error: 0.0068%) Warning: Constraint [i_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1372185017 ampere but the right hand side evaluated to 488.283458494 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0084%) Warning: Constraint [v_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission/FlightSegment.29/AircraftPerf.29/AircraftDrag.30/MotorPerf.30**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6741434128 volt but the right hand side evaluated to 36.6709222726 volt (Allowable error: 0.0001%, Actual error: 0.0088%) Warning: Constraint [i_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.118797397 ampere but the right hand side evaluated to 488.12225876 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0054%) Warning: Constraint [v_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission/FlightSegment.30/AircraftPerf.30/AircraftDrag.31/MotorPerf.31**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6442134483 volt but the right hand side evaluated to 36.6421485295 volt (Allowable error: 0.0001%, Actual error: 0.0056%) Warning: Constraint [i_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1322923046 ampere but the right hand side evaluated to 488.2403531 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0076%) Warning: Constraint [v_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission/FlightSegment.31/AircraftPerf.31/AircraftDrag.32/MotorPerf.32**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6661378417 volt but the right hand side evaluated to 36.663226212 volt (Allowable error: 0.0001%, Actual error: 0.0079%) Warning: Constraint [i_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1113203685 ampere but the right hand side evaluated to 488.056861422 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0042%) Warning: Constraint [v_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission/FlightSegment.32/AircraftPerf.32/AircraftDrag.33/MotorPerf.33**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6320610871 volt but the right hand side evaluated to 36.6304677782 volt (Allowable error: 0.0001%, Actual error: 0.0043%) Warning: Constraint [i_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1268883405 ampere but the right hand side evaluated to 488.193080238 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0067%) Warning: Constraint [v_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission/FlightSegment.33/AircraftPerf.33/AircraftDrag.34/MotorPerf.34**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6573540413 volt but the right hand side evaluated to 36.6547828916 volt (Allowable error: 0.0001%, Actual error: 0.007%) Warning: Constraint [i_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1033346408 ampere but the right hand side evaluated to 487.986966107 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [v_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission/FlightSegment.34/AircraftPerf.34/AircraftDrag.35/MotorPerf.35**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6190932676 volt but the right hand side evaluated to 36.6179996645 volt (Allowable error: 0.0001%, Actual error: 0.003%) Warning: Constraint [i_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1209900241 ampere but the right hand side evaluated to 488.141444653 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0057%) Warning: Constraint [v_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission/FlightSegment.35/AircraftPerf.35/AircraftDrag.36/MotorPerf.36**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6477751946 volt but the right hand side evaluated to 36.6455725807 volt (Allowable error: 0.0001%, Actual error: 0.006%) Warning: Constraint [i_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.0948346982 ampere but the right hand side evaluated to 487.912564701 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0015%) Warning: Constraint [v_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission/FlightSegment.36/AircraftPerf.36/AircraftDrag.37/MotorPerf.37**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6052933427 volt but the right hand side evaluated to 36.6047310037 volt (Allowable error: 0.0001%, Actual error: 0.0015%) Warning: Constraint [i_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 51.1145970877 ampere but the right hand side evaluated to 488.085515592 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0047%) Warning: Constraint [v_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission/FlightSegment.37/AircraftPerf.37/AircraftDrag.38/MotorPerf.38**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 36.6373870232 volt but the right hand side evaluated to 36.6355866205 volt (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2006 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0317 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0359 but bound is 0.0500 Using solver 'mosek' Solving for 9118 variables. Solving took 1.89 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), CL_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.2362 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.41/WingAero.41_(0,), Re_Mission.1/Climb.1/AircraftDrag.41/WingAer could cause inaccurate result because it is above upper bound. Solution is 996075.1916 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4798731087 ampere but the right hand side evaluated to 615.822674655 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.4269162713 ampere but the right hand side evaluated to 615.85860135 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.3537286416 ampere but the right hand side evaluated to 615.885329724 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.2456778787 ampere but the right hand side evaluated to 615.958884798 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 65.0888188448 ampere but the right hand side evaluated to 616.178425484 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.87%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.6835583463 volt but the right hand side evaluated to 60.7350583425 volt (Allowable error: 0.0001%, Actual error: 1.6%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.5681745964 volt but the right hand side evaluated to 60.6741581523 volt (Allowable error: 0.0001%, Actual error: 1.5%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.40320847 volt but the right hand side evaluated to 60.5822218583 volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 61.1439686919 volt but the right hand side evaluated to 60.4341862282 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.41/MotorPerf.41_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.41/M...] is not tight because the left hand side evaluated to 60.7248672717 volt but the right hand side evaluated to 60.1876711632 volt (Allowable error: 0.0001%, Actual error: 0.89%) Warning: Constraint [i_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [A]... >= 9.55*i0_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.6300875764 ampere but the right hand side evaluated to 530.632206952 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42 [V]... >= Kv_Mission.1/FlightSegment.40/AircraftPerf.40/AircraftDrag.42/MotorPerf.42**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6648408676 volt but the right hand side evaluated to 43.613865861 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [A]... >= 9.55*i0_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.619441798 ampere but the right hand side evaluated to 530.538305806 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43 [V]... >= Kv_Mission.1/FlightSegment.41/AircraftPerf.41/AircraftDrag.43/MotorPerf.43**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6463942809 volt but the right hand side evaluated to 43.5960930837 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [A]... >= 9.55*i0_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5949978737 ampere but the right hand side evaluated to 530.319809526 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44 [V]... >= Kv_Mission.1/FlightSegment.42/AircraftPerf.42/AircraftDrag.44/MotorPerf.44**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.6044826279 volt but the right hand side evaluated to 43.5554804935 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [A]... >= 9.55*i0_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5876439021 ampere but the right hand side evaluated to 530.260613114 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45 [V]... >= Kv_Mission.1/FlightSegment.43/AircraftPerf.43/AircraftDrag.45/MotorPerf.45**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5908038838 volt but the right hand side evaluated to 43.5427515585 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [A]... >= 9.55*i0_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5603527789 ampere but the right hand side evaluated to 530.017878608 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46 [V]... >= Kv_Mission.1/FlightSegment.44/AircraftPerf.44/AircraftDrag.46/MotorPerf.46**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5438330241 volt but the right hand side evaluated to 43.4973325876 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [A]... >= 9.55*i0_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5554002597 ampere but the right hand side evaluated to 529.978672669 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47 [V]... >= Kv_Mission.1/FlightSegment.45/AircraftPerf.45/AircraftDrag.47/MotorPerf.47**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.5345211133 volt but the right hand side evaluated to 43.4887160758 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [A]... >= 9.55*i0_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.525789942 ampere but the right hand side evaluated to 529.720534279 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.097%) Warning: Constraint [v_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48 [V]... >= Kv_Mission.1/FlightSegment.46/AircraftPerf.46/AircraftDrag.48/MotorPerf.48**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4827114158 volt but the right hand side evaluated to 43.4390340188 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [A]... >= 9.55*i0_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.5227609017 ampere but the right hand side evaluated to 529.693423503 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.096%) Warning: Constraint [v_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49 [V]... >= Kv_Mission.1/FlightSegment.47/AircraftPerf.47/AircraftDrag.49/MotorPerf.49**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4775426631 volt but the right hand side evaluated to 43.434022638 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [A]... >= 9.55*i0_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4902227307 ampere but the right hand side evaluated to 529.409834347 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [v_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50 [V]... >= Kv_Mission.1/FlightSegment.48/AircraftPerf.48/AircraftDrag.50/MotorPerf.50**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4206194124 volt but the right hand side evaluated to 43.3794407198 volt (Allowable error: 0.0001%, Actual error: 0.095%) Warning: Constraint [i_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [A]... >= 9.55*i0_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4897728727 ampere but the right hand side evaluated to 529.405752631 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [v_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51 [V]... >= Kv_Mission.1/FlightSegment.49/AircraftPerf.49/AircraftDrag.51/MotorPerf.51**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.4198619083 volt but the right hand side evaluated to 43.3787018268 volt (Allowable error: 0.0001%, Actual error: 0.095%) Warning: Constraint [i_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [A]... >= 9.55*i0_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4542576059 ampere but the right hand side evaluated to 529.09600803 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%) Warning: Constraint [v_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52 [V]... >= Kv_Mission.1/FlightSegment.50/AircraftPerf.50/AircraftDrag.52/MotorPerf.52**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3577952821 volt but the right hand side evaluated to 43.3191696368 volt (Allowable error: 0.0001%, Actual error: 0.089%) Warning: Constraint [i_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [A]... >= 9.55*i0_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4562080408 ampere but the right hand side evaluated to 529.112101353 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.086%) Warning: Constraint [v_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53 [V]... >= Kv_Mission.1/FlightSegment.51/AircraftPerf.51/AircraftDrag.53/MotorPerf.53**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3613736129 volt but the right hand side evaluated to 43.3225306166 volt (Allowable error: 0.0001%, Actual error: 0.09%) Warning: Constraint [i_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [A]... >= 9.55*i0_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4177752213 ampere but the right hand side evaluated to 528.777270093 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [v_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54 [V]... >= Kv_Mission.1/FlightSegment.52/AircraftPerf.52/AircraftDrag.54/MotorPerf.54**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2941698316 volt but the right hand side evaluated to 43.2580964404 volt (Allowable error: 0.0001%, Actual error: 0.083%) Warning: Constraint [i_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [A]... >= 9.55*i0_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.4222999912 ampere but the right hand side evaluated to 528.816387198 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) Warning: Constraint [v_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55 [V]... >= Kv_Mission.1/FlightSegment.53/AircraftPerf.53/AircraftDrag.55/MotorPerf.55**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.3021364814 volt but the right hand side evaluated to 43.2657113812 volt (Allowable error: 0.0001%, Actual error: 0.084%) Warning: Constraint [i_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [A]... >= 9.55*i0_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3808045138 ampere but the right hand side evaluated to 528.454236946 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.074%) Warning: Constraint [v_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56 [V]... >= Kv_Mission.1/FlightSegment.54/AircraftPerf.54/AircraftDrag.56/MotorPerf.56**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2297253171 volt but the right hand side evaluated to 43.196232258 volt (Allowable error: 0.0001%, Actual error: 0.078%) Warning: Constraint [i_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [A]... >= 9.55*i0_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.387792579 ampere but the right hand side evaluated to 528.514609162 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57 [V]... >= Kv_Mission.1/FlightSegment.55/AircraftPerf.55/AircraftDrag.57/MotorPerf.57**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.2420338223 volt but the right hand side evaluated to 43.2079948525 volt (Allowable error: 0.0001%, Actual error: 0.079%) Warning: Constraint [i_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [A]... >= 9.55*i0_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3433041407 ampere but the right hand side evaluated to 528.126412247 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [v_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58 [V]... >= Kv_Mission.1/FlightSegment.56/AircraftPerf.56/AircraftDrag.58/MotorPerf.58**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1644212192 volt but the right hand side evaluated to 43.1335278068 volt (Allowable error: 0.0001%, Actual error: 0.072%) Warning: Constraint [i_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [A]... >= 9.55*i0_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3527903904 ampere but the right hand side evaluated to 528.208608623 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) Warning: Constraint [v_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59 [V]... >= Kv_Mission.1/FlightSegment.57/AircraftPerf.57/AircraftDrag.59/MotorPerf.59**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1810764566 volt but the right hand side evaluated to 43.1494635075 volt (Allowable error: 0.0001%, Actual error: 0.073%) Warning: Constraint [i_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [A]... >= 9.55*i0_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3052594791 ampere but the right hand side evaluated to 527.793719735 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60 [V]... >= Kv_Mission.1/FlightSegment.58/AircraftPerf.58/AircraftDrag.60/MotorPerf.60**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0982223552 volt but the right hand side evaluated to 43.0699531721 volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [i_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [A]... >= 9.55*i0_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.3173026561 ampere but the right hand side evaluated to 527.898687751 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.065%) Warning: Constraint [v_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61 [V]... >= Kv_Mission.1/FlightSegment.59/AircraftPerf.59/AircraftDrag.61/MotorPerf.61**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.1192397476 volt but the right hand side evaluated to 43.0901107511 volt (Allowable error: 0.0001%, Actual error: 0.068%) Warning: Constraint [i_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [A]... >= 9.55*i0_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2666798838 ampere but the right hand side evaluated to 527.456472874 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.057%) Warning: Constraint [v_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62 [V]... >= Kv_Mission.1/FlightSegment.60/AircraftPerf.60/AircraftDrag.62/MotorPerf.62**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0311001009 volt but the right hand side evaluated to 43.0054986261 volt (Allowable error: 0.0001%, Actual error: 0.06%) Warning: Constraint [i_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [A]... >= 9.55*i0_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.28123001 ampere but the right hand side evaluated to 527.583401949 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [v_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63 [V]... >= Kv_Mission.1/FlightSegment.61/AircraftPerf.61/AircraftDrag.63/MotorPerf.63**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 43.0564601384 volt but the right hand side evaluated to 43.0298307353 volt (Allowable error: 0.0001%, Actual error: 0.062%) Warning: Constraint [i_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [A]... >= 9.55*i0_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2275263117 ampere but the right hand side evaluated to 527.114216419 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64 [V]... >= Kv_Mission.1/FlightSegment.62/AircraftPerf.62/AircraftDrag.64/MotorPerf.64**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9630087821 volt but the right hand side evaluated to 42.9401113201 volt (Allowable error: 0.0001%, Actual error: 0.053%) Warning: Constraint [i_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [A]... >= 9.55*i0_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2445865088 ampere but the right hand side evaluated to 527.263145509 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [v_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65 [V]... >= Kv_Mission.1/FlightSegment.63/AircraftPerf.63/AircraftDrag.65/MotorPerf.65**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9927126132 volt but the right hand side evaluated to 42.9686204033 volt (Allowable error: 0.0001%, Actual error: 0.056%) Warning: Constraint [i_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [A]... >= 9.55*i0_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1877315148 ampere but the right hand side evaluated to 526.766054593 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [v_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66 [V]... >= Kv_Mission.1/FlightSegment.64/AircraftPerf.64/AircraftDrag.66/MotorPerf.66**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8938929969 volt but the right hand side evaluated to 42.8737141764 volt (Allowable error: 0.0001%, Actual error: 0.047%) Warning: Constraint [i_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [A]... >= 9.55*i0_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.2073187571 ampere but the right hand side evaluated to 526.937231314 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) Warning: Constraint [v_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67 [V]... >= Kv_Mission.1/FlightSegment.65/AircraftPerf.65/AircraftDrag.67/MotorPerf.67**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.9279474891 volt but the right hand side evaluated to 42.9064148773 volt (Allowable error: 0.0001%, Actual error: 0.05%) Warning: Constraint [i_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [A]... >= 9.55*i0_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1473328415 ampere but the right hand side evaluated to 526.412806642 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [v_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68 [V]... >= Kv_Mission.1/FlightSegment.66/AircraftPerf.66/AircraftDrag.68/MotorPerf.68**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8237353921 volt but the right hand side evaluated to 42.8063288956 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [A]... >= 9.55*i0_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.169435046 ampere but the right hand side evaluated to 526.60597457 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.042%) Warning: Constraint [v_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69 [V]... >= Kv_Mission.1/FlightSegment.67/AircraftPerf.67/AircraftDrag.69/MotorPerf.69**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.8621349622 volt but the right hand side evaluated to 42.8432042178 volt (Allowable error: 0.0001%, Actual error: 0.044%) Warning: Constraint [i_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [A]... >= 9.55*i0_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.1062712594 ampere but the right hand side evaluated to 526.053682704 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.033%) Warning: Constraint [v_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70 [V]... >= Kv_Mission.1/FlightSegment.68/AircraftPerf.68/AircraftDrag.70/MotorPerf.70**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7524733041 volt but the right hand side evaluated to 42.7378734402 volt (Allowable error: 0.0001%, Actual error: 0.034%) Warning: Constraint [i_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [A]... >= 9.55*i0_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.130901423 ampere but the right hand side evaluated to 526.269017707 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.037%) Warning: Constraint [v_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71 [V]... >= Kv_Mission.1/FlightSegment.69/AircraftPerf.69/AircraftDrag.71/MotorPerf.71**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7952292904 volt but the right hand side evaluated to 42.7789396685 volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [i_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [A]... >= 9.55*i0_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0645179507 ampere but the right hand side evaluated to 525.688442186 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72 [V]... >= Kv_Mission.1/FlightSegment.70/AircraftPerf.70/AircraftDrag.72/MotorPerf.72**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.68006194 volt but the right hand side evaluated to 42.6683057455 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [A]... >= 9.55*i0_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0916895672 ampere but the right hand side evaluated to 525.92610238 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.031%) Warning: Constraint [v_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73 [V]... >= Kv_Mission.1/FlightSegment.71/AircraftPerf.71/AircraftDrag.73/MotorPerf.73**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.7271850803 volt but the right hand side evaluated to 42.7135766677 volt (Allowable error: 0.0001%, Actual error: 0.032%) Warning: Constraint [i_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [A]... >= 9.55*i0_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0220461108 ampere but the right hand side evaluated to 525.316871738 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.02%) Warning: Constraint [v_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74 [V]... >= Kv_Mission.1/FlightSegment.72/AircraftPerf.72/AircraftDrag.74/MotorPerf.74**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6064530232 volt but the right hand side evaluated to 42.5975809225 volt (Allowable error: 0.0001%, Actual error: 0.021%) Warning: Constraint [i_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [A]... >= 9.55*i0_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0517572341 ampere but the right hand side evaluated to 525.576756079 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.025%) Warning: Constraint [v_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75 [V]... >= Kv_Mission.1/FlightSegment.73/AircraftPerf.73/AircraftDrag.75/MotorPerf.75**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.6579506722 volt but the right hand side evaluated to 42.6470575081 volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [i_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [A]... >= 9.55*i0_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9788121947 ampere but the right hand side evaluated to 524.938498529 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76 [V]... >= Kv_Mission.1/FlightSegment.74/AircraftPerf.74/AircraftDrag.76/MotorPerf.76**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5315908367 volt but the right hand side evaluated to 42.5256382063 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Constraint [i_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [A]... >= 9.55*i0_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 55.0110780808 ampere but the right hand side evaluated to 525.220772758 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.018%) Warning: Constraint [v_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77 [V]... >= Kv_Mission.1/FlightSegment.75/AircraftPerf.75/AircraftDrag.77/MotorPerf.77**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5874779221 volt but the right hand side evaluated to 42.5793376906 volt (Allowable error: 0.0001%, Actual error: 0.019%) Warning: Constraint [i_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [A]... >= 9.55*i0_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9347813685 ampere but the right hand side evaluated to 524.553001255 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0068%) Warning: Constraint [v_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78 [V]... >= Kv_Mission.1/FlightSegment.76/AircraftPerf.76/AircraftDrag.78/MotorPerf.78**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.4554207437 volt but the right hand side evaluated to 42.4524236833 volt (Allowable error: 0.0001%, Actual error: 0.0071%) Warning: Constraint [i_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [A]... >= 9.55*i0_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.9696295022 ampere but the right hand side evaluated to 524.858020977 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [v_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79 [V]... >= Kv_Mission.1/FlightSegment.77/AircraftPerf.77/AircraftDrag.79/MotorPerf.79**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 42.5157172919 volt but the right hand side evaluated to 42.5103745858 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2170 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0336 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0370 but bound is 0.0500 Using solver 'mosek' Solving for 9118 variables. Solving took 1.59 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), CL_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1906 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/WingAero.82_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/WingAer could cause inaccurate result because it is above upper bound. Solution is 1169782.8944 but bound is 600000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.82/TailAero.165_(0,), Re_Mission.2/Climb.2/AircraftDrag.82/TailAe could cause inaccurate result because it is above upper bound. Solution is 1085313.8783 but bound is 1000000.0000 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500 Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.5168495353 ampere but the right hand side evaluated to 674.45473045 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.453491246 ampere but the right hand side evaluated to 674.321294991 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.3655208795 ampere but the right hand side evaluated to 674.110346811 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.2344814198 ampere but the right hand side evaluated to 673.812562111 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.95%) Warning: Constraint [i_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [A]... >= 9.55*i0_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) + Kv_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.0402878502 ampere but the right hand side evaluated to 673.430750461 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.74%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(0,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.820953192 volt but the right hand side evaluated to 71.9033732469 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(1,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.720189552 volt but the right hand side evaluated to 71.8534178622 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(2,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.5730820578 volt but the right hand side evaluated to 71.7741988601 volt (Allowable error: 0.0001%, Actual error: 1.1%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(3,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 72.3412446017 volt but the right hand side evaluated to 71.6453762201 volt (Allowable error: 0.0001%, Actual error: 0.97%) Warning: Constraint [v_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,) [V]... >= Kv_Mission.2/Climb.2/AircraftDrag.82/MotorPerf.82_(4,)**-1*omega_Mission.2/Climb.2/AircraftDrag.82/M...] is not tight because the left hand side evaluated to 71.9657521818 volt but the right hand side evaluated to 71.4291743973 volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [A]... >= 9.55*i0_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6891637979 ampere but the right hand side evaluated to 578.394544879 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83 [V]... >= Kv_Mission.2/FlightSegment.80/AircraftPerf.80/AircraftDrag.83/MotorPerf.83**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1934108048 volt but the right hand side evaluated to 52.086701414 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [A]... >= 9.55*i0_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.685953334 ampere but the right hand side evaluated to 578.363095858 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84 [V]... >= Kv_Mission.2/FlightSegment.81/AircraftPerf.81/AircraftDrag.84/MotorPerf.84**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.1879215547 volt but the right hand side evaluated to 52.0811439362 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [A]... >= 9.55*i0_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6183869836 ampere but the right hand side evaluated to 577.777178765 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85 [V]... >= Kv_Mission.2/FlightSegment.82/AircraftPerf.82/AircraftDrag.85/MotorPerf.85**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0615513295 volt but the right hand side evaluated to 51.9604162924 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [A]... >= 9.55*i0_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.6170107484 ampere but the right hand side evaluated to 577.759268997 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86 [V]... >= Kv_Mission.2/FlightSegment.83/AircraftPerf.83/AircraftDrag.86/MotorPerf.86**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 52.0598401085 volt but the right hand side evaluated to 51.9582631203 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [A]... >= 9.55*i0_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5476936053 ampere but the right hand side evaluated to 577.163225202 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87 [V]... >= Kv_Mission.2/FlightSegment.84/AircraftPerf.84/AircraftDrag.87/MotorPerf.87**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9295195025 volt but the right hand side evaluated to 51.8341895163 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [A]... >= 9.55*i0_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.5482273249 ampere but the right hand side evaluated to 577.160313608 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88 [V]... >= Kv_Mission.2/FlightSegment.85/AircraftPerf.85/AircraftDrag.88/MotorPerf.88**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.9316141011 volt but the right hand side evaluated to 51.8355379706 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [A]... >= 9.55*i0_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4762105986 ampere but the right hand side evaluated to 576.53787785 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89 [V]... >= Kv_Mission.2/FlightSegment.86/AircraftPerf.86/AircraftDrag.89/MotorPerf.89**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.7967367177 volt but the right hand side evaluated to 51.7068415395 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [A]... >= 9.55*i0_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.47897134 ampere but the right hand side evaluated to 576.555580717 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90 [V]... >= Kv_Mission.2/FlightSegment.87/AircraftPerf.87/AircraftDrag.90/MotorPerf.90**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.8028096131 volt but the right hand side evaluated to 51.7121052981 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [A]... >= 9.55*i0_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4040190257 ampere but the right hand side evaluated to 575.902919522 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91 [V]... >= Kv_Mission.2/FlightSegment.88/AircraftPerf.88/AircraftDrag.91/MotorPerf.91**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6632134621 volt but the right hand side evaluated to 51.5784774351 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [A]... >= 9.55*i0_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.4093874424 ampere but the right hand side evaluated to 575.947909288 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92 [V]... >= Kv_Mission.2/FlightSegment.89/AircraftPerf.89/AircraftDrag.92/MotorPerf.92**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.6734695566 volt but the right hand side evaluated to 51.5881434195 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [A]... >= 9.55*i0_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3322736335 ampere but the right hand side evaluated to 575.278645877 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93 [V]... >= Kv_Mission.2/FlightSegment.90/AircraftPerf.90/AircraftDrag.93/MotorPerf.93**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5295873006 volt but the right hand side evaluated to 51.450593512 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [A]... >= 9.55*i0_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.3393015165 ampere but the right hand side evaluated to 575.334625553 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94 [V]... >= Kv_Mission.2/FlightSegment.91/AircraftPerf.91/AircraftDrag.94/MotorPerf.94**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.5434447559 volt but the right hand side evaluated to 51.4634094405 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [A]... >= 9.55*i0_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.25976519 ampere but the right hand side evaluated to 574.64450446 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95 [V]... >= Kv_Mission.2/FlightSegment.92/AircraftPerf.92/AircraftDrag.95/MotorPerf.95**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.3950901216 volt but the right hand side evaluated to 51.3215869931 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [A]... >= 9.55*i0_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.2690852188 ampere but the right hand side evaluated to 574.722474473 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96 [V]... >= Kv_Mission.2/FlightSegment.93/AircraftPerf.93/AircraftDrag.96/MotorPerf.96**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.4129058954 volt but the right hand side evaluated to 51.3383697507 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [A]... >= 9.55*i0_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1865881629 ampere but the right hand side evaluated to 574.002501326 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97 [V]... >= Kv_Mission.2/FlightSegment.94/AircraftPerf.94/AircraftDrag.97/MotorPerf.97**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2597331738 volt but the right hand side evaluated to 51.1915717867 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [A]... >= 9.55*i0_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1983255536 ampere but the right hand side evaluated to 574.104668171 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98 [V]... >= Kv_Mission.2/FlightSegment.95/AircraftPerf.95/AircraftDrag.98/MotorPerf.98**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.2815612209 volt but the right hand side evaluated to 51.2124690762 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [A]... >= 9.55*i0_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 + Kv_Mission.2/Fligh...] is not tight because the left hand side evaluated to 60.1132829654 ampere but the right hand side evaluated to 573.362284578 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99 [V]... >= Kv_Mission.2/FlightSegment.96/AircraftPerf.96/AircraftDrag.99/MotorPerf.99**-1*omega_Mission.2/Fligh...] is not tight because the left hand side evaluated to 51.12377576 volt but the right hand side evaluated to 51.0612215399 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [A]... >= 9.55*i0_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.1268515237 ampere but the right hand side evaluated to 573.478623191 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [v_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100 [V]... >= Kv_Mission.2/FlightSegment.97/AircraftPerf.97/AircraftDrag.100/MotorPerf.100**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.1492655653 volt but the right hand side evaluated to 51.0854745721 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [A]... >= 9.55*i0_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0393263421 ampere but the right hand side evaluated to 572.715218251 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101 [V]... >= Kv_Mission.2/FlightSegment.98/AircraftPerf.98/AircraftDrag.101/MotorPerf.101**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 50.9868645497 volt but the right hand side evaluated to 50.9298465031 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [A]... >= 9.55*i0_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 + Kv_Mission.2/Fli...] is not tight because the left hand side evaluated to 60.0551297827 ampere but the right hand side evaluated to 572.85270429 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102 [V]... >= Kv_Mission.2/FlightSegment.99/AircraftPerf.99/AircraftDrag.102/MotorPerf.102**-1*omega_Mission.2/Fli...] is not tight because the left hand side evaluated to 51.0162340143 volt but the right hand side evaluated to 50.957961886 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [A]... >= 9.55*i0_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.964798392 ampere but the right hand side evaluated to 572.063051923 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) Warning: Constraint [v_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103 [V]... >= Kv_Mission.2/FlightSegment.100/AircraftPerf.100/AircraftDrag.103/MotorPerf.103**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8489923254 volt but the right hand side evaluated to 50.7975301465 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [A]... >= 9.55*i0_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9826321618 ampere but the right hand side evaluated to 572.218209358 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104 [V]... >= Kv_Mission.2/FlightSegment.101/AircraftPerf.101/AircraftDrag.104/MotorPerf.104**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.8821155187 volt but the right hand side evaluated to 50.8292422384 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [A]... >= 9.55*i0_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8896205065 ampere but the right hand side evaluated to 571.40481942 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) Warning: Constraint [v_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105 [V]... >= Kv_Mission.2/FlightSegment.102/AircraftPerf.102/AircraftDrag.105/MotorPerf.105**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7100603202 volt but the right hand side evaluated to 50.6641536153 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [A]... >= 9.55*i0_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.9096676267 ampere but the right hand side evaluated to 571.580796455 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.09%) Warning: Constraint [v_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106 [V]... >= Kv_Mission.2/FlightSegment.103/AircraftPerf.103/AircraftDrag.106/MotorPerf.106**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.7470292104 volt but the right hand side evaluated to 50.6996839693 volt (Allowable error: 0.0001%, Actual error: 0.093%) Warning: Constraint [i_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [A]... >= 9.55*i0_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8136203668 ampere but the right hand side evaluated to 570.737973047 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) Warning: Constraint [v_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107 [V]... >= Kv_Mission.2/FlightSegment.104/AircraftPerf.104/AircraftDrag.107/MotorPerf.107**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.5699188505 volt but the right hand side evaluated to 50.5294841601 volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [i_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [A]... >= 9.55*i0_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.8359681684 ampere but the right hand side evaluated to 570.936257793 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.08%) Warning: Constraint [v_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108 [V]... >= Kv_Mission.2/FlightSegment.105/AircraftPerf.105/AircraftDrag.108/MotorPerf.108**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.6107712461 volt but the right hand side evaluated to 50.5689311506 volt (Allowable error: 0.0001%, Actual error: 0.083%) Warning: Constraint [i_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [A]... >= 9.55*i0_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7374267265 ampere but the right hand side evaluated to 570.073613012 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [v_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109 [V]... >= Kv_Mission.2/FlightSegment.106/AircraftPerf.106/AircraftDrag.109/MotorPerf.109**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.4288460995 volt but the right hand side evaluated to 50.3942673951 volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [i_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [A]... >= 9.55*i0_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.7615471892 ampere but the right hand side evaluated to 570.285211644 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.069%) Warning: Constraint [v_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110 [V]... >= Kv_Mission.2/FlightSegment.107/AircraftPerf.107/AircraftDrag.110/MotorPerf.110**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.4732925665 volt but the right hand side evaluated to 50.4369795457 volt (Allowable error: 0.0001%, Actual error: 0.072%) Warning: Constraint [i_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [A]... >= 9.55*i0_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6602278148 ampere but the right hand side evaluated to 569.39832113 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) Warning: Constraint [v_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111 [V]... >= Kv_Mission.2/FlightSegment.108/AircraftPerf.108/AircraftDrag.111/MotorPerf.111**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.2863441354 volt but the right hand side evaluated to 50.2574846739 volt (Allowable error: 0.0001%, Actual error: 0.057%) Warning: Constraint [i_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [A]... >= 9.55*i0_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6863009561 ampere but the right hand side evaluated to 569.626291887 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.059%) Warning: Constraint [v_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112 [V]... >= Kv_Mission.2/FlightSegment.109/AircraftPerf.109/AircraftDrag.112/MotorPerf.112**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.3344789507 volt but the right hand side evaluated to 50.3036801812 volt (Allowable error: 0.0001%, Actual error: 0.061%) Warning: Constraint [i_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [A]... >= 9.55*i0_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5818366296 ampere but the right hand side evaluated to 568.709366785 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.045%) Warning: Constraint [v_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113 [V]... >= Kv_Mission.2/FlightSegment.110/AircraftPerf.110/AircraftDrag.113/MotorPerf.113**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1422568296 volt but the right hand side evaluated to 50.1188936223 volt (Allowable error: 0.0001%, Actual error: 0.047%) Warning: Constraint [i_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [A]... >= 9.55*i0_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.6102097561 ampere but the right hand side evaluated to 568.95957704 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) Warning: Constraint [v_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114 [V]... >= Kv_Mission.2/FlightSegment.111/AircraftPerf.111/AircraftDrag.114/MotorPerf.114**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.1942595103 volt but the right hand side evaluated to 50.1689863493 volt (Allowable error: 0.0001%, Actual error: 0.05%) Warning: Constraint [i_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [A]... >= 9.55*i0_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5031046288 ampere but the right hand side evaluated to 568.021618621 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.034%) Warning: Constraint [v_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115 [V]... >= Kv_Mission.2/FlightSegment.112/AircraftPerf.112/AircraftDrag.115/MotorPerf.115**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9969615511 volt but the right hand side evaluated to 49.9794877825 volt (Allowable error: 0.0001%, Actual error: 0.035%) Warning: Constraint [i_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [A]... >= 9.55*i0_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.5333084286 ampere but the right hand side evaluated to 568.286081739 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116 [V]... >= Kv_Mission.2/FlightSegment.113/AircraftPerf.113/AircraftDrag.116/MotorPerf.116**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 50.0525888204 volt but the right hand side evaluated to 50.0329146204 volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [i_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [A]... >= 9.55*i0_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4232592906 ampere but the right hand side evaluated to 567.322436852 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.023%) Warning: Constraint [v_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117 [V]... >= Kv_Mission.2/FlightSegment.114/AircraftPerf.114/AircraftDrag.117/MotorPerf.117**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.8499895383 volt but the right hand side evaluated to 49.8383162905 volt (Allowable error: 0.0001%, Actual error: 0.023%) Warning: Constraint [i_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [A]... >= 9.55*i0_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.4555331259 ampere but the right hand side evaluated to 567.605157558 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [v_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118 [V]... >= Kv_Mission.2/FlightSegment.115/AircraftPerf.115/AircraftDrag.118/MotorPerf.118**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.9093664472 volt but the right hand side evaluated to 49.8953604229 volt (Allowable error: 0.0001%, Actual error: 0.028%) Warning: Constraint [i_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [A]... >= 9.55*i0_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.342391216 ampere but the right hand side evaluated to 566.61382216 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) Warning: Constraint [v_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119 [V]... >= Kv_Mission.2/FlightSegment.116/AircraftPerf.116/AircraftDrag.119/MotorPerf.119**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7013168776 volt but the right hand side evaluated to 49.6954586786 volt (Allowable error: 0.0001%, Actual error: 0.012%) Warning: Constraint [i_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [A]... >= 9.55*i0_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.3767328335 ampere but the right hand side evaluated to 566.914704608 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.016%) Warning: Constraint [v_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120 [V]... >= Kv_Mission.2/FlightSegment.117/AircraftPerf.117/AircraftDrag.120/MotorPerf.120**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.7644457457 volt but the right hand side evaluated to 49.7561165054 volt (Allowable error: 0.0001%, Actual error: 0.017%) Warning: Variable tau_Mission.2/Aircraft.2/Wing.2/Planform.8 could cause inaccurate result because it is above upper bound. Solution is 0.2395 but bound is 0.1460 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/HorizontalTail.2/Planform.6 could cause inaccurate result because it is below lower bound. Solution is 0.0362 but bound is 0.0500 Warning: Variable tau_Mission.2/Aircraft.2/Empennage.2/VerticalTail.2/Planform.7 could cause inaccurate result because it is below lower bound. Solution is 0.0401 but bound is 0.0500 Warning: Constraint [i_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [A]... >= 9.55*i0_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 + Kv_Mission.2/F...] is not tight because the left hand side evaluated to 59.2969057956 ampere but the right hand side evaluated to 566.215202769 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.005%) Warning: Constraint [v_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122 [V]... >= Kv_Mission.2/FlightSegment.119/AircraftPerf.119/AircraftDrag.122/MotorPerf.122**-1*omega_Mission.2/F...] is not tight because the left hand side evaluated to 49.6177491745 volt but the right hand side evaluated to 49.6151501323 volt (Allowable error: 0.0001%, Actual error: 0.0052%) Using solver 'mosek' Solving for 4738 variables. Solving took 1.13 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), CL_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/WingAero.123_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Wing could cause inaccurate result because it is above upper bound. Solution is 1350804.6925 but bound is 600000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.246_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1008642.4846 but bound is 1000000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.123/TailAero.247_(0,), Re_Mission.3/Climb.3/AircraftDrag.123/Tail could cause inaccurate result because it is above upper bound. Solution is 1292032.3893 but bound is 1000000.0000 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4850203983 ampere but the right hand side evaluated to 734.385379896 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.4268843401 ampere but the right hand side evaluated to 734.13764699 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.3444145872 ampere but the right hand side evaluated to 733.758420002 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.2198352242 ampere but the right hand side evaluated to 733.184360276 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%) Warning: Constraint [i_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [A]... >= 9.55*i0_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) + Kv_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 77.0308323353 ampere but the right hand side evaluated to 732.323535416 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(0,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 85.0571723137 volt but the right hand side evaluated to 84.409146594 volt (Allowable error: 0.0001%, Actual error: 0.77%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(1,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.9749600408 volt but the right hand side evaluated to 84.3626580724 volt (Allowable error: 0.0001%, Actual error: 0.73%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(2,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.8508211394 volt but the right hand side evaluated to 84.2860537648 volt (Allowable error: 0.0001%, Actual error: 0.67%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(3,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.6551032697 volt but the right hand side evaluated to 84.1621005726 volt (Allowable error: 0.0001%, Actual error: 0.59%) Warning: Constraint [v_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,) [V]... >= Kv_Mission.3/Climb.3/AircraftDrag.123/MotorPerf.123_(4,)**-1*omega_Mission.3/Climb.3/AircraftDrag.12...] is not tight because the left hand side evaluated to 84.3396086951 volt but the right hand side evaluated to 83.9568506752 volt (Allowable error: 0.0001%, Actual error: 0.46%) Warning: Constraint [i_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [A]... >= 9.55*i0_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.694989367 ampere but the right hand side evaluated to 625.909489517 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124 [V]... >= Kv_Mission.3/FlightSegment.120/AircraftPerf.120/AircraftDrag.124/MotorPerf.124**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.2752854498 volt but the right hand side evaluated to 61.1310368421 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [A]... >= 9.55*i0_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.6041274295 ampere but the right hand side evaluated to 625.119707424 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125 [V]... >= Kv_Mission.3/FlightSegment.121/AircraftPerf.121/AircraftDrag.125/MotorPerf.125**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 61.097364276 volt but the right hand side evaluated to 60.9611394757 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [A]... >= 9.55*i0_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.5126196687 ampere but the right hand side evaluated to 624.318699754 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126 [V]... >= Kv_Mission.3/FlightSegment.122/AircraftPerf.122/AircraftDrag.126/MotorPerf.126**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.9187253131 volt but the right hand side evaluated to 60.7899980354 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [A]... >= 9.55*i0_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.4209454448 ampere but the right hand side evaluated to 623.516150839 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127 [V]... >= Kv_Mission.3/FlightSegment.123/AircraftPerf.123/AircraftDrag.127/MotorPerf.127**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.7398064997 volt but the right hand side evaluated to 60.6185631852 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [A]... >= 9.55*i0_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.329057432 ampere but the right hand side evaluated to 622.711695077 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128 [V]... >= Kv_Mission.3/FlightSegment.124/AircraftPerf.124/AircraftDrag.128/MotorPerf.128**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.5605116782 volt but the right hand side evaluated to 60.4467473491 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [A]... >= 9.55*i0_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.2366746539 ampere but the right hand side evaluated to 621.900606277 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129 [V]... >= Kv_Mission.3/FlightSegment.125/AircraftPerf.125/AircraftDrag.129/MotorPerf.129**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.3805292828 volt but the right hand side evaluated to 60.2740348617 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [A]... >= 9.55*i0_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.1444245227 ampere but the right hand side evaluated to 621.09513013 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130 [V]... >= Kv_Mission.3/FlightSegment.126/AircraftPerf.126/AircraftDrag.130/MotorPerf.130**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.2003839819 volt but the right hand side evaluated to 60.1015747435 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [A]... >= 9.55*i0_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 65.0515573627 ampere but the right hand side evaluated to 620.281801833 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131 [V]... >= Kv_Mission.3/FlightSegment.127/AircraftPerf.127/AircraftDrag.131/MotorPerf.131**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 60.0193327978 volt but the right hand side evaluated to 59.9279942184 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [A]... >= 9.55*i0_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.9582158298 ampere but the right hand side evaluated to 619.463910875 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132 [V]... >= Kv_Mission.3/FlightSegment.128/AircraftPerf.128/AircraftDrag.132/MotorPerf.132**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.8374701013 volt but the right hand side evaluated to 59.7535799628 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [A]... >= 9.55*i0_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.8636850448 ampere but the right hand side evaluated to 618.627860523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133 [V]... >= Kv_Mission.3/FlightSegment.129/AircraftPerf.129/AircraftDrag.133/MotorPerf.133**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.6539289606 volt but the right hand side evaluated to 59.5767921339 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [A]... >= 9.55*i0_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.7700302403 ampere but the right hand side evaluated to 617.814767592 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134 [V]... >= Kv_Mission.3/FlightSegment.130/AircraftPerf.130/AircraftDrag.134/MotorPerf.134**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.4709357996 volt but the right hand side evaluated to 59.4019830065 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [A]... >= 9.55*i0_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.6749605341 ampere but the right hand side evaluated to 616.980475642 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135 [V]... >= Kv_Mission.3/FlightSegment.131/AircraftPerf.131/AircraftDrag.135/MotorPerf.135**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.2859536283 volt but the right hand side evaluated to 59.2244013783 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [A]... >= 9.55*i0_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.5795939808 ampere but the right hand side evaluated to 616.14736384 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136 [V]... >= Kv_Mission.3/FlightSegment.132/AircraftPerf.132/AircraftDrag.136/MotorPerf.136**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 59.1001245806 volt but the right hand side evaluated to 59.0463506532 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [A]... >= 9.55*i0_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.4833897226 ampere but the right hand side evaluated to 615.305532641 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137 [V]... >= Kv_Mission.3/FlightSegment.133/AircraftPerf.133/AircraftDrag.137/MotorPerf.137**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.9128170932 volt but the right hand side evaluated to 58.8667292822 volt (Allowable error: 0.0001%, Actual error: 0.078%) Warning: Constraint [i_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [A]... >= 9.55*i0_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.3862501772 ampere but the right hand side evaluated to 614.45399858 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138 [V]... >= Kv_Mission.3/FlightSegment.134/AircraftPerf.134/AircraftDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.7239257271 volt but the right hand side evaluated to 58.6854266664 volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [i_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [A]... >= 9.55*i0_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.2882109242 ampere but the right hand side evaluated to 613.594052158 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139 [V]... >= Kv_Mission.3/FlightSegment.135/AircraftPerf.135/AircraftDrag.139/MotorPerf.139**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.5334171301 volt but the right hand side evaluated to 58.5025031895 volt (Allowable error: 0.0001%, Actual error: 0.053%) Warning: Constraint [i_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [A]... >= 9.55*i0_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.1893441336 ampere but the right hand side evaluated to 612.727640792 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140 [V]... >= Kv_Mission.3/FlightSegment.136/AircraftPerf.136/AircraftDrag.140/MotorPerf.140**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.3412786322 volt but the right hand side evaluated to 58.3180696995 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [A]... >= 9.55*i0_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 64.089417147 ampere but the right hand side evaluated to 611.851179674 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141 [V]... >= Kv_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.141**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 58.147248316 volt but the right hand side evaluated to 58.1317291898 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [A]... >= 9.55*i0_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 + Kv_Mission.3/F...] is not tight because the left hand side evaluated to 63.988443209 ampere but the right hand side evaluated to 610.965587173 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142 [V]... >= Kv_Mission.3/FlightSegment.138/AircraftPerf.138/AircraftDrag.142/MotorPerf.142**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 57.9512602624 volt but the right hand side evaluated to 57.9434930625 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Va.riable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/HorizontalTail.3/Planform.9 could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable tau_Mission.3/Aircraft.3/Empennage.3/VerticalTail.3/Planform.10 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Using solver 'mosek' Solving for 577 variables. Solving took 0.241 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350804.6899 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008642.4803 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292032.3840 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.484655309 ampere but the right hand side evaluated to 734.381436966 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.4265255069 ampere but the right hand side evaluated to 734.13387053 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.3440671102 ampere but the right hand side evaluated to 733.754879878 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2195111458 ampere but the right hand side evaluated to 733.181206116 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0305583252 ampere but the right hand side evaluated to 732.32103796 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V].... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0576817071 volt but the right hand side evaluated to 84.4096010285 volt (Allowable error: 0.0001%, Actual error: 0.77%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.9754373393 volt but the right hand side evaluated to 84.3630929229 volt (Allowable error: 0.0001%, Actual error: 0.73%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8512556504 volt but the right hand side evaluated to 84.2864608686 volt (Allowable error: 0.0001%, Actual error: 0.67%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6554734464 volt but the right hand side evaluated to 84.1624625444 volt (Allowable error: 0.0001%, Actual error: 0.59%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3398812419 volt but the right hand side evaluated to 83.9571362956 volt (Allowable error: 0.0001%, Actual error: 0.46%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Using solver 'mosek' Solving for 577 variables. Solving took 0.208 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350804.6899 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008642.4803 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292032.3841 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4846551701 ampere but the right hand side evaluated to 734.381435507 meter * newton * revolutions_per_minute / volt (Allowable error: 0..0001%, Actual error: 0.75%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.4265253684 ampere but the right hand side evaluated to 734.133869106 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.3440669736 ampere but the right hand side evaluated to 733.75487851 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2195110152 ampere but the right hand side evaluated to 733.181204853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0305582109 ampere but the right hand side evaluated to 732.321036907 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.057681897 volt but the right hand side evaluated to 84.4096012022 volt (Allowable error: 0.0001%, Actual error: 0.77%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.9754375213 volt but the right hand side evaluated to 84.3630930924 volt (Allowable error: 0.0001%, Actual error: 0.73%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8512558213 volt but the right hand side evaluated to 84.2864610314 volt (Allowable error: 0.0001%, Actual error: 0.67%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6554735992 volt but the right hand side evaluated to 84.162462695 volt (Allowable error: 0.0001%, Actual error: 0.59%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3398813641 volt but the right hand side evaluated to 83.9571364218 volt (Allowable error: 0.0001%, Actual error: 0.46%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Using solver 'mosek' Solving for 4738 variables. Solving took 1.26 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350804.6914 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008642.4830 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292032.3873 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4850172806 ampere but the right hand side evaluated to 734.385467439 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.4268821376 ampere but the right hand side evaluated to 734.137716055 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.344413313 ampere but the right hand side evaluated to 733.758465428 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.219834803 ampere but the right hand side evaluated to 733.184372725 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0308322245 ampere but the right hand side evaluated to 732.323506439 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0571481049 volt but the right hand side evaluated to 84.409136 volt (Allowable error: 0.0001%, Actual error: 0.77%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.974941201 volt but the right hand side evaluated to 84.3626496976 volt (Allowable error: 0.0001%, Actual error: 0.73%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8508088989 volt but the right hand side evaluated to 84.2860482207 volt (Allowable error: 0.0001%, Actual error: 0.67%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6550997387 volt but the right hand side evaluated to 84.1620989594 volt (Allowable error: 0.0001%, Actual error: 0.59%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3396152453 volt but the right hand side evaluated to 83.9568539667 volt (Allowable error: 0.0001%, Actual error: 0.46%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 65.6947886145 ampere but the right hand side evaluated to 625.906694069 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 61.2752989166 volt but the right hand side evaluated to 61.1309617517 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.6039100734 ampere but the right hand side evaluated to 625.116650023 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 61.0973715259 volt but the right hand side evaluated to 60.9610479142 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.5124208258 ampere but the right hand side evaluated to 624.315917687 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.9187349371 volt but the right hand side evaluated to 60.7899188657 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.4207652328 ampere but the right hand side evaluated to 623.513644801 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.7398183073 volt but the right hand side evaluated to 60.6184961506 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.3288943568 ampere but the right hand side evaluated to 622.709441224 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.5605251187 volt but the right hand side evaluated to 60.4466909184 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.2365453684 ampere but the right hand side evaluated to 621.898856986 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.3805478732 volt but the right hand side evaluated to 60.2740018577 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.1442884066 ampere but the right hand side evaluated to 621.093266594 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.2003985398 volt but the right hand side evaluated to 60.1015328969 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.0514314962 ampere but the right hand side evaluated to 620.28008324 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.0193470125 volt but the right hand side evaluated to 59.9279568071 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 64.9581242031 ampere but the right hand side evaluated to 619.462699365 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 59.8374886902 volt but the right hand side evaluated to 59.7535649377 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 64.8633941802 ampere but the right hand side evaluated to 618.623629497 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 59.6539059799 volt but the right hand side evaluated to 59.5766245414 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.7699412372 ampere but the right hand side evaluated to 617.813571705 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.4709494257 volt but the right hand side evaluated to 59.401962198 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.6748469503 ampere but the right hand side evaluated to 616.97889734 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.2859599506 volt but the right hand side evaluated to 59.2243586758 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.5795470366 ampere but the right hand side evaluated to 616.146774589 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.1001401377 volt but the right hand side evaluated to 59.0463521981 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.4833502321 ampere but the right hand side evaluated to 615.305040837 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.9128308395 volt but the right hand side evaluated to 58.8667316454 volt (Allowable error: 0.0001%, Actual error: 0.078%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.3862195329 ampere but the right hand side evaluated to 614.453624651 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.7239378477 volt but the right hand side evaluated to 58.685430729 volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.2881892291 ampere but the right hand side evaluated to 613.593796911 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.533427529 volt but the right hand side evaluated to 58.502508828 volt (Allowable error: 0.0001%, Actual error: 0.053%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.1893285751 ampere but the right hand side evaluated to 612.727461139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.3412866833 volt but the right hand side evaluated to 58.3180746784 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.0894080209 ampere but the right hand side evaluated to 611.851079422 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.1472539849 volt but the right hand side evaluated to 58.131733565 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 63.9884390823 ampere but the right hand side evaluated to 610.965544124 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 57.9512632071 volt but the right hand side evaluated to 57.9434956481 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 8.12 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), CL_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1644 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 1233794.1054 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/TailAero.43_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/TailAer could cause inaccurate result because it is above upper bound. Solution is 1218667.7655 but bound is 1000000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.9278086378 ampere but the right hand side evaluated to 687.174106738 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.8555106836 ampere but the right hand side evaluated to 686.986932897 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.7556489055 ampere but the right hand side evaluated to 686.703928636 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.6070188298 ampere but the right hand side evaluated to 686.300183189 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.3867945253 ampere but the right hand side evaluated to 685.764999304 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.8%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.4583204331 volt but the right hand side evaluated to 74.4446433098 volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.3595559158 volt but the right hand side evaluated to 74.4006995491 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.2143736138 volt but the right hand side evaluated to 74.3287264458 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.9849313389 volt but the right hand side evaluated to 74.2103448656 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.6115161852 volt but the right hand side evaluated to 74.0087656908 volt (Allowable error: 0.0001%, Actual error: 0.81%) Warning: Constraint [i_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.8810865874 ampere but the right hand side evaluated to 589.554509127 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.3130333564 volt but the right hand side evaluated to 54.1831622771 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7958895762 ampere but the right hand side evaluated to 588.816046542 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.1519834634 volt but the right hand side evaluated to 54.0294179248 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7099032228 ampere but the right hand side evaluated to 588.064568164 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.9903085095 volt but the right hand side evaluated to 53.8745116923 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.6237375079 ampere but the right hand side evaluated to 587.311410395 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.8283931896 volt but the right hand side evaluated to 53.7193507093 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.5373499012 ampere but the right hand side evaluated to 586.55626429 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.6661515328 volt but the right hand side evaluated to 53.5638581388 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.4504104531 ampere but the right hand side evaluated to 585.793754741 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.5033040685 volt but the right hand side evaluated to 53.407544864 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.3637045302 ampere but the right hand side evaluated to 585.038178202 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.3403199731 volt but the right hand side evaluated to 53.2515202608 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.2763267038 ampere but the right hand side evaluated to 584.274023492 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.1765328576 volt but the right hand side evaluated to 53.0944710494 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.188447268 ampere but the right hand side evaluated to 583.504763697 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0120000059 volt but the right hand side evaluated to 52.9366285104 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0994887516 ampere but the right hand side evaluated to 582.720766013 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.846292647 volt but the right hand side evaluated to 52.7771778451 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0112567349 ampere but the right hand side evaluated to 581.954072513 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.6804985036 volt but the right hand side evaluated to 52.6185936143 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.9217029795 ampere but the right hand side evaluated to 581.169354904 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.5132498277 volt but the right hand side evaluated to 52.4580299288 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.831828313 ampere but the right hand side evaluated to 580.38456535 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%) Warning: Constraint [v_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.3451099758 volt but the right hand side evaluated to 52.2968356627 volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [i_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.7411634014 ampere but the right hand side evaluated to 579.592028567 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.175718952 volt but the right hand side evaluated to 52.1343517171 volt (Allowable error: 0.0001%, Actual error: 0.079%) Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.6495626183 ampere but the right hand side evaluated to 578.789749045 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) Warning: Constraint [v_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.0049222215 volt but the right hand side evaluated to 51.97036704 volt (Allowable error: 0.0001%, Actual error: 0.066%) Warning: Constraint [i_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.5570787016 ampere but the right hand side evaluated to 577.979175943 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) Warning: Constraint [v_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.8326808169 volt but the right hand side evaluated to 51.8049305781 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.4638055645 ampere but the right hand side evaluated to 577.162464503 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [v_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.658972707 volt but the right hand side evaluated to 51.6381367381 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [A]... >= 9.55*i0_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.3694975751 ampere but the right hand side evaluated to 576.335950327 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.483578595 volt but the right hand side evaluated to 51.4696430382 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.1/FlightSegment.38/AircraftPerf.38/Aircra.ftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.2742112151 ampere but the right hand side evaluated to 575.500968637 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.3064092813 volt but the right hand side evaluated to 51.299433508 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500 Using solver 'mosek_cli' Solving for 4738 variables. Solving took 1.52 seconds. Warning: Variable [CL_Mission/Climb/AircraftDrag/WingAero_(0,), CL_Mission/Climb/AircraftDrag/WingAero_(1,), CL_Missio could cause inaccurate result because it is below lower bound. Solution is 1.1513 but bound is 0.9465 Warning: Variable [Re_Mission/Climb/AircraftDrag/WingAero_(0,), Re_Mission/Climb/AircraftDrag/WingAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1350803.2858 but bound is 600000.0000 Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero_(0,), Re_Mission/Climb/AircraftDrag/TailAero_(1,), Re_Missio could cause inaccurate result because it is above upper bound. Solution is 1008646.6099 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1292036.2239 but bound is 1000000.0000 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(0,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(0,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)*Q_M...] is not tight because the left hand side evaluated to 77.4850488745 ampere but the right hand side evaluated to 734.385298061 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.75%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(1,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(1,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)*Q_M...] is not tight because the left hand side evaluated to 77.4268794482 ampere but the right hand side evaluated to 734.137816343 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(2,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(2,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)*Q_M...] is not tight because the left hand side evaluated to 77.3443863713 ampere but the right hand side evaluated to 733.758470359 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.66%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(3,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(3,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)*Q_M...] is not tight because the left hand side evaluated to 77.2198076579 ampere but the right hand side evaluated to 733.183974901 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.57%) Warning: Constraint [i_Mission/Climb/AircraftDrag/MotorPerf_(4,) [A]... >= 9.55*i0_Mission/Climb/AircraftDrag/MotorPerf_(4,) + Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)*Q_M...] is not tight because the left hand side evaluated to 77.0308506959 ampere but the right hand side evaluated to 732.323127431 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.45%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(0,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(0,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(0,) + R...] is not tight because the left hand side evaluated to 85.0571173803 volt but the right hand side evaluated to 84.4091098586 volt (Allowable error: 0.0001%, Actual error: 0.77%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(1,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(1,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(1,) + R...] is not tight because the left hand side evaluated to 84.974906903 volt but the right hand side evaluated to 84.3625930251 volt (Allowable error: 0.0001%, Actual error: 0.73%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(2,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(2,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(2,) + R...] is not tight because the left hand side evaluated to 84.8508492102 volt but the right hand side evaluated to 84.2860319189 volt (Allowable error: 0.0001%, Actual error: 0.67%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(3,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(3,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(3,) + R...] is not tight because the left hand side evaluated to 84.6550699606 volt but the right hand side evaluated to 84.1621054377 volt (Allowable error: 0.0001%, Actual error: 0.59%) Warning: Constraint [v_Mission/Climb/AircraftDrag/MotorPerf_(4,) [V]... >= Kv_Mission/Climb/AircraftDrag/MotorPerf_(4,)**-1*omega_Mission/Climb/AircraftDrag/MotorPerf_(4,) + R...] is not tight because the left hand side evaluated to 84.3396416976 volt but the right hand side evaluated to 83.9568933953 volt (Allowable error: 0.0001%, Actual error: 0.46%) Warning: Constraint [i_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [A]... >= 9.55*i0_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 + Kv_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 65.6948147999 ampere but the right hand side evaluated to 625.906433661 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1 [V]... >= Kv_Mission/FlightSegment/AircraftPerf/AircraftDrag.1/MotorPerf.1**-1*omega_Mission/FlightSegment/Air...] is not tight because the left hand side evaluated to 61.2753107009 volt but the right hand side evaluated to 61.1309802723 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [A]... >= 9.55*i0_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.603890461 ampere but the right hand side evaluated to 625.116510034 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2 [V]... >= Kv_Mission/FlightSegment.1/AircraftPerf.1/AircraftDrag.2/MotorPerf.2**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 61.0973809327 volt but the right hand side evaluated to 60.9610562443 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [A]... >= 9.55*i0_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.5124368376 ampere but the right hand side evaluated to 624.316029817 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3 [V]... >= Kv_Mission/FlightSegment.2/AircraftPerf.2/AircraftDrag.3/MotorPerf.3**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.9187494454 volt but the right hand side evaluated to 60.7899457 volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [i_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [A]... >= 9.55*i0_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.4207835982 ampere but the right hand side evaluated to 623.513747587 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [v_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4 [V]... >= Kv_Mission/FlightSegment.3/AircraftPerf.3/AircraftDrag.4/MotorPerf.4**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.7397898632 volt but the right hand side evaluated to 60.618490689 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [A]... >= 9.55*i0_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.3289319382 ampere but the right hand side evaluated to 622.709673848 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5 [V]... >= Kv_Mission/FlightSegment.4/AircraftPerf.4/AircraftDrag.5/MotorPerf.5**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.5605081533 volt but the right hand side evaluated to 60.4466969306 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [A]... >= 9.55*i0_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.2365568703 ampere but the right hand side evaluated to 621.899187678 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6 [V]... >= Kv_Mission/FlightSegment.5/AircraftPerf.5/AircraftDrag.6/MotorPerf.6**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.3805479945 volt but the right hand side evaluated to 60.2739781632 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [A]... >= 9.55*i0_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.1443124206 ampere but the right hand side evaluated to 621.093303304 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7 [V]... >= Kv_Mission/FlightSegment.6/AircraftPerf.6/AircraftDrag.7/MotorPerf.7**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.200400192 volt but the right hand side evaluated to 60.1015257676 volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [i_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [A]... >= 9.55*i0_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 65.0514177829 ampere but the right hand side evaluated to 620.27988106 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8 [V]... >= Kv_Mission/FlightSegment.7/AircraftPerf.7/AircraftDrag.8/MotorPerf.8**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 60.019349386 volt but the right hand side evaluated to 59.9279855819 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [A]... >= 9.55*i0_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 + Kv_Mission/FlightSegment...] is not tight because the left hand side evaluated to 64.9581359441 ampere but the right hand side evaluated to 619.46299136 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9 [V]... >= Kv_Mission/FlightSegment.8/AircraftPerf.8/AircraftDrag.9/MotorPerf.9**-1*omega_Mission/FlightSegment...] is not tight because the left hand side evaluated to 59.837466807 volt but the right hand side evaluated to 59.7535514429 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [A]... >= 9.55*i0_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 + Kv_Mission/FlightSegme...] is not tight because the left hand side evaluated to 64.8634311277 ampere but the right hand side evaluated to 618.624231002 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10 [V]... >= Kv_Mission/FlightSegment.9/AircraftPerf.9/AircraftDrag.10/MotorPerf.10**-1*omega_Mission/FlightSegme...] is not tight because the left hand side evaluated to 59.6539281687 volt but the right hand side evaluated to 59.5765917627 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [A]... >= 9.55*i0_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.769965465 ampere but the right hand side evaluated to 617.813707923 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11 [V]... >= Kv_Mission/FlightSegment.10/AircraftPerf.10/AircraftDrag.11/MotorPerf.11**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.4709524959 volt but the right hand side evaluated to 59.4019726831 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [A]... >= 9.55*i0_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.6748235622 ampere but the right hand side evaluated to 616.979069193 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12 [V]... >= Kv_Mission/FlightSegment.11/AircraftPerf.11/AircraftDrag.12/MotorPerf.12**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.2859294236 volt but the right hand side evaluated to 59.2243279816 volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [i_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [A]... >= 9.55*i0_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.5795630965 ampere but the right hand side evaluated to 616.146788661 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.088%) Warning: Constraint [v_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13 [V]... >= Kv_Mission/FlightSegment.12/AircraftPerf.12/AircraftDrag.13/MotorPerf.13**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 59.1001226674 volt but the right hand side evaluated to 59.0463574101 volt (Allowable error: 0.0001%, Actual error: 0.091%) Warning: Constraint [i_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [A]... >= 9.55*i0_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.483346715 ampere but the right hand side evaluated to 615.305412796 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14 [V]... >= Kv_Mission/FlightSegment.13/AircraftPerf.13/AircraftDrag.14/MotorPerf.14**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.9128362588 volt but the right hand side evaluated to 58.8667345516 volt (Allowable error: 0.0001%, Actual error: 0.078%) Warning: Constraint [i_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [A]... >= 9.55*i0_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.3862434972 ampere but the right hand side evaluated to 614.453270768 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.063%) Warning: Constraint [v_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15 [V]... >= Kv_Mission/FlightSegment.14/AircraftPerf.14/AircraftDrag.15/MotorPerf.15**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.7239118038 volt but the right hand side evaluated to 58.6854800991 volt (Allowable error: 0.0001%, Actual error: 0.065%) Warning: Constraint [i_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [A]... >= 9.55*i0_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.2881935951 ampere but the right hand side evaluated to 613.593838092 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) Warning: Constraint [v_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16 [V]... >= Kv_Mission/FlightSegment.15/AircraftPerf.15/AircraftDrag.16/MotorPerf.16**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.5334274238 volt but the right hand side evaluated to 58.5025542353 volt (Allowable error: 0.0001%, Actual error: 0.053%) Warning: Constraint [i_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [A]... >= 9.55*i0_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.1893301601 ampere but the right hand side evaluated to 612.727151495 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.038%) Warning: Constraint [v_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17 [V]... >= Kv_Mission/FlightSegment.16/AircraftPerf.16/AircraftDrag.17/MotorPerf.17**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.3412855688 volt but the right hand side evaluated to 58.3180929577 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [A]... >= 9.55*i0_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 64.0894010487 ampere but the right hand side evaluated to 611.850972455 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18 [V]... >= Kv_Mission/FlightSegment.17/AircraftPerf.17/AircraftDrag.18/MotorPerf.18**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 58.1472740521 volt but the right hand side evaluated to 58.1317140621 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [A]... >= 9.55*i0_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 63.9884117142 ampere but the right hand side evaluated to 610.965348838 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19 [V]... >= Kv_Mission/FlightSegment.18/AircraftPerf.18/AircraftDrag.19/MotorPerf.19**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 57.9512418942 volt but the right hand side evaluated to 57.9434957772 volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2605 but bound is 0.1460 Warning: Variable tau_Mission/Aircraft/Empennage/HorizontalTail/Planform could cause inaccurate result because it is below lower bound. Solution is 0.0371 but bound is 0.0500 Warning: Variable tau_Mission/Aircraft/Empennage/VerticalTail/Planform.1 could cause inaccurate result because it is below lower bound. Solution is 0.0431 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 9 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), CL_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.1644 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/WingAero.21_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/WingAer could cause inaccurate result because it is above upper bound. Solution is 1233788.4076 but bound is 600000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.21/TailAero.43_(0,), Re_Mission.1/Climb.1/AircraftDrag.21/TailAer could cause inaccurate result because it is above upper bound. Solution is 1218669.1980 but bound is 1000000.0000 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500 Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.9278065177 ampere but the right hand side evaluated to 687.17425883 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.8554980045 ampere but the right hand side evaluated to 686.986823198 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.7556088009 ampere but the right hand side evaluated to 686.704162667 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.6069756102 ampere but the right hand side evaluated to 686.300025677 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [i_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [A]... >= 9.55*i0_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) + Kv_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 72.386802727 ampere but the right hand side evaluated to 685.764999224 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.8%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(0,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.4582859806 volt but the right hand side evaluated to 74.4446350664 volt (Allowable error: 0.0001%, Actual error: 1.4%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(1,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.3595757042 volt but the right hand side evaluated to 74.4006949388 volt (Allowable error: 0.0001%, Actual error: 1.3%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(2,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 75.2143472006 volt but the right hand side evaluated to 74.3286747933 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(3,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.9849180014 volt but the right hand side evaluated to 74.2103574307 volt (Allowable error: 0.0001%, Actual error: 1%) Warning: Constraint [v_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,) [V]... >= Kv_Mission.1/Climb.1/AircraftDrag.21/MotorPerf.21_(4,)**-1*omega_Mission.1/Climb.1/AircraftDrag.21/M...] is not tight because the left hand side evaluated to 74.6115260525 volt but the right hand side evaluated to 74.0087383665 volt (Allowable error: 0.0001%, Actual error: 0.81%) Warning: Constraint [i_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [A]... >= 9.55*i0_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.8809884973 ampere but the right hand side evaluated to 589.553101064 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [v_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22 [V]... >= Kv_Mission.1/FlightSegment.20/AircraftPerf.20/AircraftDrag.22/MotorPerf.22**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.3130212382 volt but the right hand side evaluated to 54.18304199 volt (Allowable error: 0.0001%, Actual error: 0.24%) Warning: Constraint [i_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [A]... >= 9.55*i0_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7957752206 ampere but the right hand side evaluated to 588.814076673 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [v_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23 [V]... >= Kv_Mission.1/FlightSegment.21/AircraftPerf.21/AircraftDrag.23/MotorPerf.23**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 54.151950873 volt but the right hand side evaluated to 54.0293441617 volt (Allowable error: 0.0001%, Actual error: 0.23%) Warning: Constraint [i_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [A]... >= 9.55*i0_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.7098153434 ampere but the right hand side evaluated to 588.062969162 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.21%) Warning: Constraint [v_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24 [V]... >= Kv_Mission.1/FlightSegment.22/AircraftPerf.22/AircraftDrag.24/MotorPerf.24**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.9902783607 volt but the right hand side evaluated to 53.8743994879 volt (Allowable error: 0.0001%, Actual error: 0.22%) Warning: Constraint [i_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [A]... >= 9.55*i0_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.6236669201 ampere but the right hand side evaluated to 587.310173516 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [v_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25 [V]... >= Kv_Mission.1/FlightSegment.23/AircraftPerf.23/AircraftDrag.25/MotorPerf.25**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.8283887537 volt but the right hand side evaluated to 53.7192733842 volt (Allowable error: 0.0001%, Actual error: 0.2%) Warning: Constraint [i_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [A]... >= 9.55*i0_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.5372695373 ampere but the right hand side evaluated to 586.554612422 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [v_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26 [V]... >= Kv_Mission.1/FlightSegment.24/AircraftPerf.24/AircraftDrag.26/MotorPerf.26**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.6661259071 volt but the right hand side evaluated to 53.5638134216 volt (Allowable error: 0.0001%, Actual error: 0.19%) Warning: Constraint [i_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [A]... >= 9.55*i0_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.4503173279 ampere but the right hand side evaluated to 585.792500531 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [v_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27 [V]... >= Kv_Mission.1/FlightSegment.25/AircraftPerf.25/AircraftDrag.27/MotorPerf.27**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.5032821169 volt but the right hand side evaluated to 53.4075012405 volt (Allowable error: 0.0001%, Actual error: 0.18%) Warning: Constraint [i_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [A]... >= 9.55*i0_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.3636107091 ampere but the right hand side evaluated to 585.037419822 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [v_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28 [V]... >= Kv_Mission.1/FlightSegment.26/AircraftPerf.26/AircraftDrag.28/MotorPerf.28**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.3402923705 volt but the right hand side evaluated to 53.2514491424 volt (Allowable error: 0.0001%, Actual error: 0.17%) Warning: Constraint [i_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [A]... >= 9.55*i0_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.2762298375 ampere but the right hand side evaluated to 584.272563332 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [v_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29 [V]... >= Kv_Mission.1/FlightSegment.27/AircraftPerf.27/AircraftDrag.29/MotorPerf.29**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.176522896 volt but the right hand side evaluated to 53.0944525676 volt (Allowable error: 0.0001%, Actual error: 0.15%) Warning: Constraint [i_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [A]... >= 9.55*i0_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.1883615083 ampere but the right hand side evaluated to 583.503921246 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [v_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30 [V]... >= Kv_Mission.1/FlightSegment.28/AircraftPerf.28/AircraftDrag.30/MotorPerf.30**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 53.0119839364 volt but the right hand side evaluated to 52.9365796818 volt (Allowable error: 0.0001%, Actual error: 0.14%) Warning: Constraint [i_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [A]... >= 9.55*i0_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0993360802 ampere but the right hand side evaluated to 582.718558689 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [v_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31 [V]... >= Kv_Mission.1/FlightSegment.29/AircraftPerf.29/AircraftDrag.31/MotorPerf.31**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.8462629862 volt but the right hand side evaluated to 52.7770576258 volt (Allowable error: 0.0001%, Actual error: 0.13%) Warning: Constraint [i_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [A]... >= 9.55*i0_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 61.0112333196 ampere but the right hand side evaluated to 581.953740219 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [v_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32 [V]... >= Kv_Mission.1/FlightSegment.30/AircraftPerf.30/AircraftDrag.32/MotorPerf.32**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.6804806084 volt but the right hand side evaluated to 52.6185536045 volt (Allowable error: 0.0001%, Actual error: 0.12%) Warning: Constraint [i_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [A]... >= 9.55*i0_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.9216736156 ampere but the right hand side evaluated to 581.168477196 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.1%) Warning: Constraint [v_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33 [V]... >= Kv_Mission.1/FlightSegment.31/AircraftPerf.31/AircraftDrag.33/MotorPerf.33**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.513222761 volt but the right hand side evaluated to 52.4580064608 volt (Allowable error: 0.0001%, Actual error: 0.11%) Warning: Constraint [i_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [A]... >= 9.55*i0_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.8318195539 ampere but the right hand side evaluated to 580.383820841 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.089%) Warning: Constraint [v_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34 [V]... >= Kv_Mission.1/FlightSegment.32/AircraftPerf.32/AircraftDrag.34/MotorPerf.34**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.3451349576 volt but the right hand side evaluated to 52.2968339873 volt (Allowable error: 0.0001%, Actual error: 0.092%) Warning: Constraint [i_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [A]... >= 9.55*i0_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.7411261533 ampere but the right hand side evaluated to 579.591722477 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.076%) Warning: Constraint [v_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35 [V]... >= Kv_Mission.1/FlightSegment.33/AircraftPerf.33/AircraftDrag.35/MotorPerf.35**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.1757068214 volt but the right hand side evaluated to 52.1343252574 volt (Allowable error: 0.0001%, Actual error: 0.079%) Warning: Constraint [i_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [A]... >= 9.55*i0_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.6495369154 ampere but the right hand side evaluated to 578.789539308 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) Warning: Constraint [v_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36 [V]... >= Kv_Mission.1/FlightSegment.34/AircraftPerf.34/AircraftDrag.36/MotorPerf.36**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 52.0049548698 volt but the right hand side evaluated to 51.9703441171 volt (Allowable error: 0.0001%, Actual error: 0.067%) Warning: Constraint [i_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [A]... >= 9.55*i0_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.5570563027 ampere but the right hand side evaluated to 577.978925092 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) Warning: Constraint [v_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37 [V]... >= Kv_Mission.1/FlightSegment.35/AircraftPerf.35/AircraftDrag.37/MotorPerf.37**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.8326883777 volt but the right hand side evaluated to 51.8049576872 volt (Allowable error: 0.0001%, Actual error: 0.054%) Warning: Constraint [i_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [A]... >= 9.55*i0_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 + Kv_Mission.1/Fligh...] is not tight because the left hand side eva. ---------------------------------------------------------------------- Ran 6 tests in 206.575s OK Generating XML reports... luated to 60.4638097438 ampere but the right hand side evaluated to 577.162058503 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.039%) Warning: Constraint [v_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38 [V]... >= Kv_Mission.1/FlightSegment.36/AircraftPerf.36/AircraftDrag.38/MotorPerf.38**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.6589777792 volt but the right hand side evaluated to 51.6381372512 volt (Allowable error: 0.0001%, Actual error: 0.04%) Warning: Constraint [i_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [A]... >= 9.55*i0_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.3694993652 ampere but the right hand side evaluated to 576.335771748 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.026%) Warning: Constraint [v_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39 [V]... >= Kv_Mission.1/FlightSegment.37/AircraftPerf.37/AircraftDrag.39/MotorPerf.39**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.4835840219 volt but the right hand side evaluated to 51.4696429733 volt (Allowable error: 0.0001%, Actual error: 0.027%) Warning: Constraint [i_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 + Kv_Mission.1/Fligh...] is not tight because the left hand side evaluated to 60.2741908698 ampere but the right hand side evaluated to 575.500644951 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) Warning: Constraint [v_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission.1/FlightSegment.38/AircraftPerf.38/AircraftDrag.40/MotorPerf.40**-1*omega_Mission.1/Fligh...] is not tight because the left hand side evaluated to 51.3064256157 volt but the right hand side evaluated to 51.2994476997 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.1/Aircraft.1/Wing.1/Planform.5 could cause inaccurate result because it is above upper bound. Solution is 0.2427 but bound is 0.1460 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/HorizontalTail.1/Planform.3 could cause inaccurate result because it is below lower bound. Solution is 0.0274 but bound is 0.0500 Warning: Variable tau_Mission.1/Aircraft.1/Empennage.1/VerticalTail.1/Planform.4 could cause inaccurate result because it is below lower bound. Solution is 0.0428 but bound is 0.0500 Cloning into 'gplibrary'... Requirement already satisfied: pandas in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (0.22.0) Requirement already satisfied: python-dateutil in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2.7.2) Requirement already satisfied: numpy>=1.9.0 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (1.14.2) Requirement already satisfied: pytz>=2011k in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from pandas) (2018.4) Requirement already satisfied: six>=1.5 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from python-dateutil->pandas) (1.11.0) Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to /tmp/pip-req-build-SCgtm3 Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages Requirement already satisfied: numpy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpfit==0.1) (1.0.1) Requirement already satisfied: gpkit in /jenkins/workspace/gplibrary_PR_Models/mosek/gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkit->gpfit==0.1) (1.3.2) Building wheels for collected packages: gpfit Running setup.py bdist_wheel for gpfit: started Running setup.py bdist_wheel for gpfit: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-jJeI8C/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Processing /jenkins/workspace/gplibrary_PR_Models/mosek/gplibrary Requirement already satisfied: numpy>=1.12 in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.14.2) Requirement already satisfied: scipy in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (1.0.1) Requirement already satisfied: pint in /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/lib/python2.7/site-packages (from gpkitmodels==0.0.0.0) (0.8.1) Building wheels for collected packages: gpkitmodels Running setup.py bdist_wheel for gpkitmodels: started Running setup.py bdist_wheel for gpkitmodels: finished with status 'done' Stored in directory: /tmp/pip-ephem-wheel-cache-Ye3OOX/wheels/63/f8/98/93b45f0bf8ab3367cc8d67f05c8a0e19f356c1a33a86d02692 Successfully built gpkitmodels Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Not uninstalling gpkitmodels at /jenkins/workspace/gplibrary_PR_Models/mosek, outside environment /jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit Can't uninstall 'gpkitmodels'. No files were found to uninstall. Successfully installed gpkitmodels-0.0.0.0 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 6.140s OK Generating XML reports... adding test for 'gpkitmodels/GP/aircraft/wing/wing_test.py' adding test for 'gpkitmodels/GP/aircraft/tail/tail_tests.py' adding test for 'gpkitmodels/GP/aircraft/fuselage/test_fuselage.py' adding test for 'gpkitmodels/GP/aircraft/prop/prop_test.py' adding test for 'gpkitmodels/GP/aircraft/motor/motor_test.py' Using solver 'mosek' Solving for 11 variables. Solving took 0.197 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.24 seconds. Using solver 'mosek' Solving for 8 variables. Solving took 0.0317 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.0311 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.0208 seconds. Using solver 'mosek_cli' Solving for 8 variables. Solving took 0.225 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.223 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.24 seconds. Using solver 'mosek' Solving for 13 variables. Solving took 0.0328 seconds. Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.227 seconds. Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220953.3481 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499787.9721 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 2223878.3856 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 2223877.9562 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.1020 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.1579 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656769.2019 but bound is 700000.0000 Cloning into 'eVTOL'... Running tests... ---------------------------------------------------------------------- .. ---------------------------------------------------------------------- Ran 2 tests in 1.620s OK Generating XML reports... adding test for 'aircraft_models.py' USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '--no-cache-dir', '--no-deps', '-e', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/shopping.git'] attempt 1 SETTINGS defaultdict(, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/turbofan.git'] attempt 1 SETTINGS defaultdict(, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/turbofan.git'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/solar.git'] attempt 1 SETTINGS defaultdict(, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'pandas'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['python', '/jenkins/workspace/gplibrary_PR_Models/mosek/venv2_gpkit/bin/pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(, {}) [Execution node] check if [reynolds] is in [[windows10x64, windows7x64]] Run condition [Execution node ] preventing perform for step [Execute Windows batch command] [xUnit] [INFO] - Starting to record. [xUnit] [INFO] - Processing JUnit [xUnit] [INFO] - [JUnit] - 8 test report file(s) were found with the pattern '**/test_reports/*.xml, **/test_reports_nounits/*.xml' relative to '/jenkins/workspace/gplibrary_PR_Models/mosek' for the testing framework 'JUnit'. [xUnit] [INFO] - Check 'Failed Tests' threshold. [xUnit] [INFO] - Check 'Skipped Tests' threshold. [xUnit] [INFO] - Setting the build status to SUCCESS [xUnit] [INFO] - Stopping recording. [WS-CLEANUP] Deleting project workspace...[WS-CLEANUP] done Finished: SUCCESS