Started by upstream project "gplibrary_PR_Models" build number 85 originally caused by: GitHub pull request #163 of commit 6c6cc701787d73771d32d65f2b0cfe10c4aafcd0, 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 69b8ab2a2ef26feabc1b357a142f7fb198b5a058 (refs/remotes/origin/pr/163/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 69b8ab2a2ef26feabc1b357a142f7fb198b5a058 # 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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origin/sigeq_paper Seen branch in repository origin/simple_HT_sizing Seen branch in repository origin/simple_flight_profile Seen branch in repository origin/standard_atmosphere Seen branch in repository origin/sutherland Seen branch in repository origin/troposphere Seen branch in repository origin/vectorizeplanform Seen branch in repository origin/wide_body Seen branch in repository origin/wvl Seen 201 remote branches > git show-ref --tags -d # timeout=10 Checking out Revision 69b8ab2a2ef26feabc1b357a142f7fb198b5a058 (origin/pr/163/merge, origin/master) > git config core.sparsecheckout # timeout=10 > git checkout -f 69b8ab2a2ef26feabc1b357a142f7fb198b5a058 # timeout=3 Commit message: "Merge 6c6cc701787d73771d32d65f2b0cfe10c4aafcd0 into 37b19bb4ed498761eb51296a13946b1a52fa40aa" Using 'Changelog to branch' strategy. 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 163: allow for outboard loads on wing as signomial 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/jenkins4332170759600623338.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 0.730s OK Generating XML reports... adding test for 'test.py' Using solver 'mosek' Solving for 25 variables. Solving took 0.0663 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.0314 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.437 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-9Ng56V 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-XzyMg3/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-FdupFj/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 26.485s 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 0.25 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 0.96 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 1.06 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 0.377 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 2.32 seconds. Warning: Variable Re_Mission.1/FlightSegment.11/AircraftPerf.11/WingAero.11 could cause inaccurate result because it is below lower bound. Solution is 134553.0580 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 0.525 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 3.18 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-JGEWOF 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-kSSjiB/wheels/4d/4b/2e/9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 42.702s OK Generating XML reports... adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -5.023021928951543e-14. Allowing negative dual variable(s) as small as -7.357742887181828e-14. Allowing negative dual variable(s) as small as -1.5164215369511957e-13. Allowing negative dual variable(s) as small as -1.4890085692220723e-13. Solving took 4 GP solves and 2.79 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.1377305188005096e-14. Allowing negative dual variable(s) as small as -7.40627177642228e-14. Allowing negative dual variable(s) as small as -1.5064251929208794e-13. Allowing negative dual variable(s) as small as -1.4909991644107556e-13. Solving took 4 GP solves and 2.92 seconds. Allowing negative dual variable(s) as small as -5.188297708125233e-13. Allowing negative dual variable(s) as small as -1.43054144918775e-12. Allowing negative dual variable(s) as small as -4.451369828295526e-13. Allowing negative dual variable(s) as small as -4.446738116614668e-13. Allowing negative dual variable(s) as small as -1.2966744648498785e-12. Allowing negative dual variable(s) as small as -1.091298275704422e-12. Allowing negative dual variable(s) as small as -1.0907411042079818e-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 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 -2.41020072061065e-14. Allowing negative dual variable(s) as small as -5.6961012152384265e-12. Allowing negative dual variable(s) as small as -2.0879096032395267e-11. Allowing negative dual variable(s) as small as -2.088073862309172e-11. Solving took 4 GP solves and 3.21 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.29 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.184741524999481e-13. Allowing negative dual variable(s) as small as -1.429037443934078e-12. Allowing negative dual variable(s) as small as -4.4269622689885324e-13. Allowing negative dual variable(s) as small as -4.4383420549909403e-13. Allowing negative dual variable(s) as small as -1.2967866797747307e-12. Allowing negative dual variable(s) as small as -1.090790543827047e-12. Allowing negative dual variable(s) as small as -1.0914456187796628e-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 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 -2.436208030811058e-14. Allowing negative dual variable(s) as small as -5.696152269964034e-12. Allowing negative dual variable(s) as small as -2.0879152623222338e-11. Allowing negative dual variable(s) as small as -2.0880872586063948e-11. Solving took 4 GP solves and 2.57 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.94 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-BA4yMT/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 1.536s 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-cubVkA 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-5THikj/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 2519604.07265 force_pound * meter but the right hand side evaluated to 2468460.52803 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 32774.4969406 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 2.21510116799 meter but the right hand side evaluated to 1.96396129948 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 48608.8154319 newton but the right hand side evaluated to 48529.6585404 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 49704.4416103 newton but the right hand side evaluated to 49411.2061145 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 18949.0237768 newton but the right hand side evaluated to 18923.0271102 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 16591.9584092 newton but the right hand side evaluated to 16565.7504303 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 1002816.32464 joule / kilogram but the right hand side evaluated to 1.15243619113 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 895045.536514 joule / kilogram but the right hand side evaluated to 0.89747435102 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 1072947.60989 joule / kilogram but the right hand side evaluated to 1.19571307502 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 596870.972806 joule / kilogram but the right hand side evaluated to 0.615557396547 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 786925.816767 joule / kilogram but the right hand side evaluated to 0.790364833651 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 18.3465565608 meter but the right hand side evaluated to 16.3967786897 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 11.085408843197737 but the right hand side evaluated to 4.680790321312465 (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 9.791744781437151 but the right hand side evaluated to 4.680790317363997 (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 8.229131944406806 but the right hand side evaluated to 4.680790322521103 (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 18.4249278829 meter but the right hand side evaluated to 18.1659868483 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 18.4249278829 meter but the right hand side evaluated to 18.2854603391 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 0.31012120035150925 but the right hand side evaluated to 0.19292694955487855 (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 0.24134264810400197 but the right hand side evaluated to 0.17650152531053886 (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 7.275041676711991 but the right hand side evaluated to 4.615987191805532 (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 7.45367005331976 but the right hand side evaluated to 4.6463454711537775 (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 2504977.98529 force_pound * meter but the right hand side evaluated to 2454471.18771 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 32774.4713512 force_pound but the right hand side evaluated to 32399.9999977 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 2.21510116762 meter but the right hand side evaluated to 1.96383073053 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 982256.919925 joule / kilogram but the right hand side evaluated to 1.20547073595 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 1151137.28191 joule / kilogram but the right hand side evaluated to 1.88379417241 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 18.4111631438 meter but the right hand side evaluated to 16.4524825094 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 11.089309212364519 but the right hand side evaluated to 4.731321153932028 (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 9.749133416590258 but the right hand side evaluated to 4.7313211395807215 (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 8.197833769508152 but the right hand side evaluated to 4.73132115901863 (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 18.4749979181 meter but the right hand side evaluated to 18.2223432887 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 18.4749979181 meter but the right hand side evaluated to 18.3384489703 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 0.3092783006342552 but the right hand side evaluated to 0.19273731118596452 (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 0.24172948078563117 but the right hand side evaluated to 0.17660010965093437 (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 7.4302227208883345 but the right hand side evaluated to 4.666980842715267 (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 7.495476940730811 but the right hand side evaluated to 4.696717028845417 (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 2481455.73997 force_pound * meter but the right hand side evaluated to 2426089.72417 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 32774.4966737 force_pound but the right hand side evaluated to 32399.999999 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 2.21510116798 meter but the right hand side evaluated to 1.83119998962 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 1203383.86484 joule / kilogram but the right hand side evaluated to 1.66382937276 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 18.4693766826 meter but the right hand side evaluated to 16.6432023935 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 11.04730864849687 but the right hand side evaluated to 4.801810915261806 (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 9.670708591725418 but the right hand side evaluated to 4.801810910444976 (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 8.221376013408577 but the right hand side evaluated to 4.801810916838062 (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 18.6280060374 meter but the right hand side evaluated to 18.3449855499 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 18.6280060374 meter but the right hand side evaluated to 18.4743840633 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 0.3268338648427065 but the right hand side evaluated to 0.19660320073497703 (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 0.25275797329287464 but the right hand side evaluated to 0.17939072675237544 (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 7.455618881872759 but the right hand side evaluated to 4.729223987145624 (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 7.548868489947029 but the right hand side evaluated to 4.762582124799092 (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 2455568.31982 force_pound * meter but the right hand side evaluated to 2407712.27885 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 32774.4960131 force_pound but the right hand side evaluated to 32399.9999987 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 2.21510116797 meter but the right hand side evaluated to 1.9955213076 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 1227634.02079 joule / kilogram but the right hand side evaluated to 1.72359902468 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 677538.96192 joule / kilogram but the right hand side evaluated to 0.679181980182 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 18.4156361804 meter but the right hand side evaluated to 16.4239734633 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 10.974970561234747 but the right hand side evaluated to 4.762555432985479 (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 9.752897444473899 but the right hand side evaluated to 4.762555425581236 (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 8.158718945023269 but the right hand side evaluated to 4.76255543512098 (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 18.4488731861 meter but the right hand side evaluated to 18.2046637608 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 18.4488731861 meter but the right hand side evaluated to 18.3176181446 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 0.3059466624187097 but the right hand side evaluated to 0.1919893639638003 (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 0.23933825616595872 but the right hand side evaluated to 0.17598569166902692 (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 7.504818402298985 but the right hand side evaluated to 4.699784204571504 (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 7.527659546546523 but the right hand side evaluated to 4.728944931506322 (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 2436785.56112 force_pound * meter but the right hand side evaluated to 2390898.61264 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 32774.4697336 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 2.21510116795 meter but the right hand side evaluated to 2.03201149239 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 1233975.50345 joule / kilogram but the right hand side evaluated to 1.62326376344 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 18.4095778389 meter but the right hand side evaluated to 16.3813512592 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 10.931050507378936 but the right hand side evaluated to 4.787718038965283 (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 9.873362838496067 but the right hand side evaluated to 4.7877180312329966 (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 8.154647230487718 but the right hand side evaluated to 4.787718041137225 (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 18.4102715373 meter but the right hand side evaluated to 18.1746820549 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 18.4102715373 meter but the right hand side evaluated to 18.2839322921 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 0.3020985066309949 but the right hand side evaluated to 0.1911201520655525 (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 0.23685355271228214 but the right hand side evaluated to 0.17534404709426005 (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 7.536485569274902 but the right hand side evaluated to 4.726722222621196 (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 7.551399928505735 but the right hand side evaluated to 4.755135128137167 (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 2418324.20559 force_pound * meter but the right hand side evaluated to 2374883.02797 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 32774.4709322 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 2.21510116785 meter but the right hand side evaluated to 2.08235846797 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 1244507.22237 joule / kilogram but the right hand side evaluated to 1.5592764496 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 664750.723261 joule / kilogram but the right hand side evaluated to 0.6674021993 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 18.4000464499 meter but the right hand side evaluated to 16.3223740251 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 10.904038595642865 but the right hand side evaluated to 4.789501979365057 (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 10.025980932199257 but the right hand side evaluated to 4.789501968485124 (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 8.145554969986367 but the right hand side evaluated to 4.789501982118275 (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 18.3617959544 meter but the right hand side evaluated to 18.1374274338 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 18.3617959544 meter but the right hand side evaluated to 18.2416865668 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 0.29596087497449375 but the right hand side evaluated to 0.18972173443329512 (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 0.2329761357529172 but the right hand side evaluated to 0.17433488777288722 (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 7.565345483474593 but the right hand side evaluated to 4.731316847321391 (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 7.583817791524762 but the right hand side evaluated to 4.758513813054395 (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 2405738.41994 force_pound * meter but the right hand side evaluated to 2358168.42357 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 32774.4045159 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 2.21510116801 meter but the right hand side evaluated to 1.97490956381 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 1245747.3076 joule / kilogram but the right hand side evaluated to 1.3577299086 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 18.4441341895 meter but the right hand side evaluated to 16.4749786446 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 10.933107567571522 but the right hand side evaluated to 4.831717258733745 (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 10.19213804068147 but the right hand side evaluated to 4.831717235494585 (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 8.195656196704078 but the right hand side evaluated to 4.831717263562035 (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 18.4861310614 meter but the right hand side evaluated to 18.2368508379 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 18.4861310614 meter but the right hand side evaluated to 18.351864999 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 0.31020252366899825 but the right hand side evaluated to 0.19294190657082624 (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 0.24191511164256774 but the right hand side evaluated to 0.17664668279659754 (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 7.54212857954635 but the right hand side evaluated to 4.7669778589172545 (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 7.597029536464197 but the right hand side evaluated to 4.797041709547996 (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 2391783.13025 force_pound * meter but the right hand side evaluated to 2346060.50962 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 32774.3849056 force_pound but the right hand side evaluated to 32399.9999953 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 2.21510116719 meter but the right hand side evaluated to 2.01208061101 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 1263255.2045 joule / kilogram but the right hand side evaluated to 1.32933947134 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 643003.484788 joule / kilogram but the right hand side evaluated to 0.644588082431 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 18.4391927348 meter but the right hand side evaluated to 16.4333074804 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 10.927056273754511 but the right hand side evaluated to 4.8270961485410675 (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 10.33284099254655 but the right hand side evaluated to 4.827096047172643 (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 8.188195604168406 but the right hand side evaluated to 4.827096173070751 (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 18.4531758554 meter but the right hand side evaluated to 18.2123844019 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 18.4531758554 meter but the right hand side evaluated to 18.3237433309 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 0.30544756128225536 but the right hand side evaluated to 0.1918757343941459 (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 0.23885821397777907 but the right hand side evaluated to 0.17586253963798767 (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 7.554288347408919 but the right hand side evaluated to 4.764561118507336 (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 7.6178359604085255 but the right hand side evaluated to 4.793693845535543 (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 2376281.38547 force_pound * meter but the right hand side evaluated to 2334599.89502 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 32774.5685419 force_pound but the right hand side evaluated to 32399.9999971 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 2.21510116786 meter but the right hand side evaluated to 2.09817340737 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 1283641.26861 joule / kilogram but the right hand side evaluated to 1.28936149733 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 18.4146016057 meter but the right hand side evaluated to 16.3183405481 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 10.93746335379538 but the right hand side evaluated to 4.824378893912811 (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 10.571344881494232 but the right hand side evaluated to 4.824378878079547 (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 8.193850847341013 but the right hand side evaluated to 4.824378898190993 (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 18.3565580203 meter but the right hand side evaluated to 18.1377546049 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/CruiseSegmen. ---------------------------------------------------------------------- Ran 1 test in 114.296s OK Generating XML reports... t/CruiseP/AircraftP.1_(1, 0) [m]...] is not tight because the left hand side evaluated to 18.3565580203 meter but the right hand side evaluated to 18.2401748803 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 0.29417323930165384 but the right hand side evaluated to 0.18931098041973 (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 0.23165850623231599 but the right hand side evaluated to 0.17398969776968584 (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 7.620071564081682 but the right hand side evaluated to 4.767020067998717 (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 7.6893912351194755 but the right hand side evaluated to 4.793938477618511 (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 111 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-Wb7LVl 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-YGkbam/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-5FS6aU 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-gSCzi0/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-AsppaB/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 9073 variables. Solving took 2.75 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 1.3000 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 796269.5176 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 0.1885 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 0.0315 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 0.0352 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 65.7609005055 ampere but the right hand side evaluated to 616.348265673 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 65.6904100315 ampere but the right hand side evaluated to 616.348266433 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 65.5943352119 ampere but the right hand side evaluated to 616.348267133 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 65.4468189041 ampere but the right hand side evaluated to 616.348267883 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 65.2157694838 ampere but the right hand side evaluated to 616.348268895 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 40.8361575014 volt but the right hand side evaluated to 40.0442877093 volt (Allowable error: 0.0001%, Actual error: 2%) 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 40.7564339544 volt but the right hand side evaluated to 40.0109034576 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 40.6357804503 volt but the right hand side evaluated to 39.9534916223 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 40.4485542327 volt but the right hand side evaluated to 39.8631072239 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 40.1471960704 volt but the right hand side evaluated to 39.7128058563 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 48.4046083817 ampere but the right hand side evaluated to 462.161099059 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 32.6524147448 volt but the right hand side evaluated to 32.6473131673 volt (Allowable error: 0.0001%, Actual error: 0.016%) 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 48.376958523 ampere but the right hand side evaluated to 461.909866954 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 32.6357630197 volt but the right hand side evaluated to 32.63160971 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 48.4032724905 ampere but the right hand side evaluated to 462.148949629 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 32.6515961471 volt but the right hand side evaluated to 32.6465395506 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 48.378977435 ampere but the right hand side evaluated to 461.928210077 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 32.6369829574 volt but the right hand side evaluated to 32.6327603187 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 48.4012428858 ampere but the right hand side evaluated to 462.130502254 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 32.6503693105 volt but the right hand side evaluated to 32.6453818662 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 48.3803022923 ampere but the right hand side evaluated to 461.940251653 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 32.6377899459 volt but the right hand side evaluated to 32.6335221342 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 48.3985104692 ampere but the right hand side evaluated to 462.105681136 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 32.6487388839 volt but the right hand side evaluated to 32.6438455983 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 48.3809332223 ampere but the right hand side evaluated to 461.945991596 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381826286 volt but the right hand side evaluated to 32.6338937106 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 48.3950918511 ampere but the right hand side evaluated to 462.074619349 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 32.646685393 volt but the right hand side evaluated to 32.6419093832 volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 48.3808926677 ampere but the right hand side evaluated to 461.945610865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381385826 volt but the right hand side evaluated to 32.6338501389 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 48.3909830891 ampere but the right hand side evaluated to 462.037282148 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 32.6442062245 volt but the right hand side evaluated to 32.63957081 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 48.3801430654 ampere but the right hand side evaluated to 461.938800856 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 32.6376870464 volt but the right hand side evaluated to 32.6334243809 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 48.3861615476 ampere but the right hand side evaluated to 461.993481418 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 32.6413140224 volt but the right hand side evaluated to 32.636844619 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 48.3786889425 ampere but the right hand side evaluated to 461.925595436 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 32.6368188102 volt but the right hand side evaluated to 32.6326065284 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 48.3806415653 ampere but the right hand side evaluated to 461.943330004 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6379872446 volt but the right hand side evaluated to 32.6337074769 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 48.3765444482 ampere but the right hand side evaluated to 461.906106241 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 32.6355147986 volt but the right hand side evaluated to 32.6313757624 volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 48.3744123365 ampere but the right hand side evaluated to 461.886735073 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 32.6342252683 volt but the right hand side evaluated to 32.6301595323 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 48.3736800771 ampere but the right hand side evaluated to 461.880088291 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 32.6337931058 volt but the right hand side evaluated to 32.6297529209 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 48.3674679674 ampere but the right hand side evaluated to 461.823643137 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 32.6300216631 volt but the right hand side evaluated to 32.6261945657 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 48.3701100533 ampere but the right hand side evaluated to 461.847652734 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 32.6316318273 volt but the right hand side evaluated to 32.6277142553 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 48.3597904304 ampere but the right hand side evaluated to 461.753901062 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 32.625379199 volt but the right hand side evaluated to 32.6218167526 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 48.3658230766 ampere but the right hand side evaluated to 461.808701505 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 32.6290301166 volt but the right hand side evaluated to 32.6252596512 volt (Allowable error: 0.0001%, Actual error: 0.012%) 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 48.3513889394 ampere but the right hand side evaluated to 461.677577486 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0096%) 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 32.6202753777 volt but the right hand side evaluated to 32.6170021805 volt (Allowable error: 0.0001%, Actual error: 0.01%) 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 48.3608068102 ampere but the right hand side evaluated to 461.763127966 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) 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 32.6259866812 volt but the right hand side evaluated to 32.6223886798 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 48.3422456993 ampere but the right hand side evaluated to 461.594519551 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 32.6147095652 volt but the right hand side evaluated to 32.6117514729 volt (Allowable error: 0.0001%, Actual error: 0.0091%) 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 48.3550561028 ampere but the right hand side evaluated to 461.710882956 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0099%) 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 32.6224922092 volt but the right hand side evaluated to 32.619091981 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 48.3323597498 ampere but the right hand side evaluated to 461.504711413 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0077%) 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 32.6086649864 volt but the right hand side evaluated to 32.6060473637 volt (Allowable error: 0.0001%, Actual error: 0.008%) 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 48.3485608055 ampere but the right hand side evaluated to 461.651875946 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0093%) 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 32.6185403694 volt but the right hand side evaluated to 32.6153637329 volt (Allowable error: 0.0001%, Actual error: 0.0097%) 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 48.3217150031 ampere but the right hand side evaluated to 461.408013287 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0066%) 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 32.6021364126 volt but the right hand side evaluated to 32.5998856858 volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 48.3413127552 ampere but the right hand side evaluated to 461.586032089 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) 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 32.6141214699 volt but the right hand side evaluated to 32.6111944761 volt (Allowable error: 0.0001%, Actual error: 0.009%) 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 48.3103004186 ampere but the right hand side evaluated to 461.304325585 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 32.5951124808 volt but the right hand side evaluated to 32.5932554868 volt (Allowable error: 0.0001%, Actual error: 0.0057%) 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 48.333301283 ampere but the right hand side evaluated to 461.513255209 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0078%) 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 32.6092263179 volt but the right hand side evaluated to 32.6065754488 volt (Allowable error: 0.0001%, Actual error: 0.0081%) 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 48.2980770633 ampere but the right hand side evaluated to 461.193320677 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 32.5876045768 volt but the right hand side evaluated to 32.586171416 volt (Allowable error: 0.0001%, Actual error: 0.0044%) 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 48.3245063632 ampere but the right hand side evaluated to 461.433371495 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 32.6038520194 volt but the right hand side evaluated to 32.6015050407 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 48.2850803656 ampere but the right hand side evaluated to 461.075275971 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 32.5795566285 volt but the right hand side evaluated to 32.5785729005 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 48.3149434622 ampere but the right hand side evaluated to 461.346497074 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0059%) 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 32.5979631541 volt but the right hand side evaluated to 32.5959455264 volt (Allowable error: 0.0001%, Actual error: 0.0062%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 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 48.2712740105 ampere but the right hand side evaluated to 460.949883317 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 32.5709738133 volt but the right hand side evaluated to 32.5704679549 volt (Allowable error: 0.0001%, Actual error: 0.0016%) 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 48.3045581077 ampere but the right hand side evaluated to 461.25217492 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0049%) 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 32.5915832004 volt but the right hand side evaluated to 32.5899250144 volt (Allowable error: 0.0001%, Actual error: 0.0051%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 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 0.0315 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 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2933606501 ampere but the right hand side evaluated to 461.150477076 meter * newton * r/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) evolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [v_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.584677047 volt but the right hand side evaluated to 32.5834064179 volt (Allowable error: 0.0001%, Actual error: 0.0039%) Using solver 'mosek' Solving for 9073 variables. Solving took 2 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 1.2824 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 882794.0512 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 0.1991 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 0.0328 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 0.0367 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 83.6082501361 ampere but the right hand side evaluated to 779.784457036 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.4%) 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 83.5016049752 ampere but the right hand side evaluated to 779.78445709 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 83.3557342749 ampere but the right hand side evaluated to 779.784457139 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.1%) 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 83.1310518324 ampere but the right hand side evaluated to 779.78445719 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 82.7771607055 ampere but the right hand side evaluated to 779.78445726 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 38.5657784348 volt but the right hand side evaluated to 37.5903753645 volt (Allowable error: 0.0001%, Actual error: 2.6%) 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 38.4804161843 volt but the right hand side evaluated to 37.5596574844 volt (Allowable error: 0.0001%, Actual error: 2.5%) 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 38.3522610731 volt but the right hand side evaluated to 37.5062528295 volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 38.1536666771 volt but the right hand side evaluated to 37.4222340767 volt (Allowable error: 0.0001%, Actual error: 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 37.8404671739 volt but the right hand side evaluated to 37.2880130212 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 55.5643547165 ampere but the right hand side evaluated to 529.997456324 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 34.8016714064 volt but the right hand side evaluated to 34.7600660206 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 55.5215905091 ampere but the right hand side evaluated to 529.597242647 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 34.8064946635 volt but the right hand side evaluated to 34.7654161793 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 55.4297936903 ampere but the right hand side evaluated to 528.736313164 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 34.8139614785 volt but the right hand side evaluated to 34.7738930949 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 55.3865482317 ampere but the right hand side evaluated to 528.334967021 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 34.8251830415 volt but the right hand side evaluated to 34.7858768589 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 55.2803693726 ampere but the right hand side evaluated to 527.339737882 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 34.8358035223 volt but the right hand side evaluated to 34.797711553 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 55.2491924421 ampere but the right hand side evaluated to 527.050521106 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 34.8446142422 volt but the right hand side evaluated to 34.8070828827 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 55.1198991116 ampere but the right hand side evaluated to 525.841583904 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.8644856605 volt but the right hand side evaluated to 34.8286409225 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 55.1083669037 ampere but the right hand side evaluated to 525.733352092 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.8655615146 volt but the right hand side evaluated to 34.8298403774 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 54.9644157244 ampere but the right hand side evaluated to 524.386974572 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8887668818 volt but the right hand side evaluated to 34.8549077392 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.9628318135 ampere but the right hand side evaluated to 524.372071025 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8888551103 volt but the right hand side evaluated to 34.8550104357 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.8041523031 ampere but the right hand side evaluated to 522.887320001 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9154329499 volt but the right hand side evaluated to 34.8836103376 volt (Allowable error: 0.0001%, Actual error: 0.091%) 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 54.8153896074 ampere but the right hand side evaluated to 522.991996182 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9124990764 volt but the right hand side evaluated to 34.8805007514 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 54.6402494234 ampere but the right hand side evaluated to 521.352819871 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 34.9436464962 volt but the right hand side evaluated to 34.9138653969 volt (Allowable error: 0.0001%, Actual error: 0.085%) 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 54.6618712957 ampere but the right hand side evaluated to 521.555064688 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 34.939369086 volt but the right hand side evaluated to 34.9093052816 volt (Allowable error: 0.0001%, Actual error: 0.086%) 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 54.4714788324 ampere but the right hand side evaluated to 519.772106502 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 34.974224993 volt but the right hand side evaluated to 34.946515392 volt (Allowable error: 0.0001%, Actual error: 0.079%) 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 54.505572908 ampere but the right hand side evaluated to 520.091136006 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) 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 34.9671230211 volt but the right hand side evaluated to 34.9389733979 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 54.2975981942 ampere but the right hand side evaluated to 518.142749512 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 35.007296087 volt but the right hand side evaluated to 34.9816808124 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 54.3440884956 ampere but the right hand side evaluated to 518.578095245 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.071%) 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 34.997402462 volt but the right hand side evaluated to 34.9712055143 volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 54.1178385958 ampere but the right hand side evaluated to 516.457465396 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) 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 35.0433552112 volt but the right hand side evaluated to 35.0198619278 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 54.1762495543 ampere but the right hand side evaluated to 517.005002853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) 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 35.0309835536 volt but the right hand side evaluated to 35.0067937026 volt (Allowable error: 0.0001%, Actual error: 0.069%) 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 53.9307720132 ampere but the right hand side evaluated to 514.702838009 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 35.0833583727 volt but the right hand side evaluated to 35.0620309513 volt (Allowable error: 0.0001%, Actual error: 0.061%) 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 54.0027375612 ampere but the right hand side evaluated to 515.377843599 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.06%) 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 35.0673494495 volt but the right hand side evaluated to 35.0451862309 volt (Allowable error: 0.0001%, Actual error: 0.063%) 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 53.7355628567 ampere but the right hand side evaluated to 512.870792448 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) 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 35.1278482444 volt but the right hand side evaluated to 35.108725251 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 53.8220254586 ampere but the right hand side evaluated to 513.682294238 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) 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 35.1075263661 volt but the right hand side evaluated to 35.0874280982 volt (Allowable error: 0.0001%, Actual error: 0.057%) 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 53.5316994218 ampere but the right hand side evaluated to 510.956171515 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.046%) 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 35.1771423516 volt but the right hand side evaluated to 35.1602448104 volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 53.633620409 ampere but the right hand side evaluated to 511.91345999 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) 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 35.1518182971 volt but the right hand side evaluated to 35.133811349 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 53.3157432977 ampere but the right hand side evaluated to 508.926604144 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 35.233607074 volt but the right hand side evaluated to 35.218990035 volt (Allowable error: 0.0001%, Actual error: 0.042%) 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 53.4353998876 ampere but the right hand side evaluated to 510.051299648 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.043%) 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 35.2016698189 volt but the right hand side evaluated to 35.1857977221 volt (Allowable error: 0.0001%, Actual error: 0.045%) 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 53.0857762944 ampere but the right hand side evaluated to 506.763516375 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 35.2985535803 volt but the right hand side evaluated to 35.286256199 volt (Allowable error: 0.0001%, Actual error: 0.035%) 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 53.2255177789 ampere but the right hand side evaluated to 508.07813661 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 35.25833582 volt but the right hand side evaluated to 35.2446404687 volt (Allowable error: 0.0001%, Actual error: 0.039%) 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 52.8375034196 ampere but the right hand side evaluated to 504.425911817 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) 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 35.3749666968 volt but the right hand side evaluated to 35.3650319103 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 53.0011118134 ampere but the right hand side evaluated to 505.966632866 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 35.3237883732 volt but the right hand side evaluated to 35.3123133102 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 52.563700871 ampere but the right hand side evaluated to 501.844822711 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 35.4679071128 volt but the right hand side evaluated to 35.4603822977 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 52.7581499005 ampere but the right hand side evaluated to 503.678195045 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 35.400830603 volt but the right hand side evaluated to 35.3916154803 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 52.2509579596 ampere but the right hand side evaluated to 498.892089797 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 35.5868288423 volt but the right hand side evaluated to 35.5817592518 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 52.4890816267 ampere but the right hand side evaluated to 501.14074064 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.019%) 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 35.4947553429 volt but the right hand side evaluated to 35.4878444212 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 51.86390163 ampere but the right hand side evaluated to 495.229870921 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 35.756772671 volt but the right hand side evaluated to 35.7542076311 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 52.1785642518 ampere but the right hand side evaluated to 498.207800498 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 35.6163802771 volt but the right hand side evaluated to 35.6118258513 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 0.1991 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 0.0328 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 0.0367 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 0.1991 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 0.0328 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 0.0367 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 2.3 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 1.2351 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 988744.2411 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 0.2106 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 0.0340 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 0.0369 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 99.8053665527 ampere but the right hand side evaluated to 936.513511236 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 99.7125436974 ampere but the right hand side evaluated to 936.513511243 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 99.586600469 ampere but the right hand side evaluated to 936.513511252 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 99.3939698935 ampere but the right hand side evaluated to 936.513511258 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_(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 99.0931287278 ampere but the right hand side evaluated to 936.513511269 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 38.2500478044 volt but the right hand side evaluated to 37.5140775039 volt (Allowable error: 0.0001%, Actual error: 2%) 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 38.1813138061 volt but the right hand side evaluated to 37.4858738795 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 38.0772361466 volt but the right hand side evaluated to 37.4367677753 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.9163410431 volt but the right hand side evaluated to 37.3595016651 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.6635831337 volt but the right hand side evaluated to 37.236168007 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 65.8562215351 ampere but the right hand side evaluated to 627.638333336 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 35.0193095114 volt but the right hand side evaluated to 34.9458478712 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 65.8479913174 ampere but the right hand side evaluated to 627.558656574 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 35.0179368132 volt but the right hand side evaluated to 34.9444051704 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 65.5672494796 ampere but the right hand side evaluated to 624.946002356 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 35.0396670695 volt but the right hand side evaluated to 34.9698517518 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 65.5696397725 ampere but the right hand side evaluated to 624.963584909 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 35.0363821042 volt but the right hand side evaluated to 34.9662638842 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 65.2731994905 ampere but the right hand side evaluated to 622.207809132 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 35.0630821893 volt but the right hand side evaluated to 34.9970940042 volt (Allowable error: 0.0001%, Actual error: 0.19%) 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 65.2860176722 ampere but the right hand side evaluated to 622.321267294 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 35.0579710451 volt but the right hand side evaluated to 34.9914701765 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 64.9803638959 ampere but the right hand side evaluated to 619.476638201 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 35.085271093 volt but the right hand side evaluated to 35.0228761189 volt (Allowable error: 0.0001%, Actual error: 0.18%) 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 65.0010582089 ampere but the right hand side evaluated to 619.664498472 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 35.0799879539 volt but the right hand side evaluated to 35.0170355183 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 64.6877567431 ampere but the right hand side evaluated to 616.744243231 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 35.1068155261 volt but the right hand side evaluated to 35.0478445514 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 64.7128698064 ampere but the right hand side evaluated to 616.976997702 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 35.1036069599 volt but the right hand side evaluated to 35.0442373332 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 64.3852325919 ampere but the right hand side evaluated to 613.92362267 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 35.134355185 volt but the right hand side evaluated to 35.079216636 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 64.4226778331 ampere but the right hand side evaluated to 614.268957367 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 35.1279305164 volt but the right hand side evaluated to 35.072090515 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 64.0818778278 ampere but the right hand side evaluated to 611.091990606 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 35.1617694909 volt but the right hand side evaluated to 35.1103151712 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 64.1264193784 ampere but the right hand side evaluated to 611.5051871 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 35.1555600405 volt but the right hand side evaluated to 35.1034089568 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 63.7762695396 ampere but the right hand side evaluated to 608.237018747 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 35.1899182141 volt but the right hand side evaluated to 35.1420726802 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.8267917834 ampere but the right hand side evaluated to 608.708418919 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 35.1846203417 volt but the right hand side evaluated to 35.1361412482 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.4629766511 ampere but the right hand side evaluated to 605.311285206 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 35.2222934966 volt but the right hand side evaluated to 35.1782462829 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.5245935112 ampere but the right hand side evaluated to 605.885310138 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 35.2144993589 volt but the right hand side evaluated to 35.169617842 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.1454823017 ampere but the right hand side evaluated to 602.344448806 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 35.2565026349 volt but the right hand side evaluated to 35.2162307818 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 63.214783932 ampere but the right hand side evaluated to 602.991662685 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 35.2484290878 volt but the right hand side evaluated to 35.2073068519 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 62.8221043508 ampere but the right hand side evaluated to 599.321391909 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 35.2935607932 volt but the right hand side evaluated to 35.2570991711 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 62.9011824588 ampere but the right hand side evaluated to 600.060249433 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 35.2838034205 volt but the right hand side evaluated to 35.2463821441 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 62.4925674046 ampere but the right hand side evaluated to 596.239163505 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 35.333555297 volt but the right hand side evaluated to 35.3009209572 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 62.5797041061 ampere but the right hand side evaluated to 597.054794143 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 35.3232150509 volt but the right hand side evaluated to 35.2896029284 volt (Allowable error: 0.0001%, Actual error: 0.095%) 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 62.1579158283 ampere but the right hand side evaluated to 593.106501301 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 35.3757102557 volt but the right hand side evaluated to 35.3468457245 volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 62.2517354433 ampere but the right hand side evaluated to 593.986843343 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 35.3656596007 volt but the right hand side evaluated to 35.3358642119 volt (Allowable error: 0.0001%, Actual error: 0.084%) 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 61.806793222 ampere but the right hand side evaluated to 589.821788997 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 35.4273542698 volt but the right hand side evaluated to 35.4026266949 volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 61.915757072 ampere but the right hand side evaluated to 590.842333692 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 35.4120389867 volt but the right hand side evaluated to 35.3860971056 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 61.4495417765 ampere but the right hand side evaluated to 586.475879466 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 35.4816257653 volt but the right hand side evaluated to 35.4609176344 volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 61.5712475457 ampere but the right hand side evaluated to 587.61589472 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 35.4625994225 volt but the right hand side evaluated to 35.4405259079 volt (Allowable error: 0.0001%, Actual error: 0.062%) 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 61.0866663498 ampere but the right hand side evaluated to 583.072866746 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 35.538106568 volt but the right hand side evaluated to 35.5212533586 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 61.2164351004 ampere but the right hand side evaluated to 584.2908523 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 35.5184021741 volt but the right hand side evaluated to 35.5002296955 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 60.7005544387 ampere but the right hand side evaluated to 579.453010675 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 35.6081765134 volt but the right hand side evaluated to 35.5955521605 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 60.8482210985 ampere but the right hand side evaluated to 580.838257055 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 35.5813694136 volt but the right hand side evaluated to 35.5671747966 volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 60.3007127041 ampere but the right hand side evaluated to 575.700001852 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.022%) 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 35.6855319219 volt but the right hand side evaluated to 35.6770671144 volt (Allowable error: 0.0001%, Actual error: 0.024%) 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 60.4639074713 ampere but the right hand side evaluated to 577.232228207 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 35.6531550472 volt but the right hand side evaluated to 35.6430131217 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 59.8791609332 ampere but the right hand side evaluated to 571.739266548 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 35.7752527497 volt but the right hand side evaluated to 35.7709879609 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 60.0608454758 ampere but the right hand side evaluated to 573.44677771 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 35.7353731495 volt but the right hand side evaluated to 35.7293202128 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 0.2106 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 0.0340 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 0.0369 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 59.6316175062 ampere but the right hand side evaluated to 569.411442625 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 35.832710034 volt but the right hand side evaluated to 35.8308142901 volt (Allowable error: 0.0001%, Actual error: 0.0053%) Using solver 'mosek' Solving for 4713 variables. Solving took 1.06 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 1.2058 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 1064456.8435 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 0.2186 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 0.0349 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 0.0382 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 111.917810713 ampere but the right hand side evaluated to 1056.06638268 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.846541257 ampere but the right hand side evaluated to 1056.06638269 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750519055 ampere but the right hand side evaluated to 1056.0663827 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604592276 ampere but the right hand side evaluated to 1056.06638272 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378510957 ampere but the right hand side evaluated to 1056.06638273 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2100218668 volt but the right hand side evaluated to 37.7037019531 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552399 volt but the right hand side evaluated to 37.6768755058 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0707771602 volt but the right hand side evaluated to 37.630062704 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401425879 volt but the right hand side evaluated to 37.5563497138 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350477929 volt but the right hand side evaluated to 37.4386740022 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3931414697 ampere but the right hand side evaluated to 699.26296302 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 35.2475642196 volt but the right hand side evaluated to 35.1620428599 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 73.0289058934 ampere but the right hand side evaluated to 695.876983177 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 35.2658446392 volt but the right hand side evaluated to 35.1848748505 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6669896055 ampere but the right hand side evaluated to 692.506049518 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 35.2825857881 volt but the right hand side evaluated to 35.2058330309 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3031326078 ampere but the right hand side evaluated to 689.116210078 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 35.3004820175 volt but the right hand side evaluated to 35.2279643094 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9369645103 ampere but the right hand side evaluated to 685.704028273 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 35.3196517498 volt but the right hand side evaluated to 35.251393136 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 71.569996075 ampere but the right hand side evaluated to 682.281341155 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 35.3389918789 volt but the right hand side evaluated to 35.2748778148 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 71.1963086389 ampere but the right hand side evaluated to 678.799478768 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 35.3622192681 volt but the right hand side evaluated to 35.302558772 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211720807 ampere but the right hand side evaluated to 675.300815276 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 35.385790114 volt but the right hand side evaluated to 35.3304652137 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4426766308 ampere but the right hand side evaluated to 671.769302015 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 35.4108203797 volt but the right hand side evaluated to 35.3598315695 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 70.0648709307 ampere but the right hand side evaluated to 668.238307761 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 35.4345972488 volt but the right hand side evaluated to 35.3876533127 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 69.6718344631 ampere but the right hand side evaluated to 664.574165758 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 35.4671817665 volt but the right hand side evaluated to 35.4250080041 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 69.2794499924 ampere but the right hand side evaluated to 660.909016887 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 35.4982825422 volt but the right hand side evaluated to 35.4605262938 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8780417025 ampere but the right hand side evaluated to 657.160735543 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 35.5339390198 volt but the right hand side evaluated to 35.5008211904 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4705014199 ampere but the right hand side evaluated to 653.352897113 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.5721736181 volt but the right hand side evaluated to 35.5436916655 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.0565748959 ampere but the right hand side evaluated to 649.482597561 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 35.6130141687 volt but the right hand side evaluated to 35.5891398005 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.6342938152 ampere but the right hand side evaluated to 645.53201312 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 35.6575621906 volt but the right hand side evaluated to 35.6383246653 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.2008049908 ampere but the right hand side evaluated to 641.475148139 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 35.7074556611 volt but the right hand side evaluated to 35.6929605185 volt (Allowable error: 0.0001%, Actual error: 0.041%) Warning: Constraint [i_Mission.3/FlightSegment.137/AircraftPerf.137/AircraftDrag.141/MotorPerf.1.41 [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 66.7560125597 ampere but the right hand side evaluated to 637.309632528 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 35.762587156 volt but the right hand side evaluated to 35.7528599036 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 66.2964788144 ampere but the right hand side evaluated to 633.003357774 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 35.8249152363 volt but the right hand side evaluated to 35.8200288692 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 1.81 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 1.3000 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 796269.5178 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 0.1885 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 0.0315 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 0.0352 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 65.7608999693 ampere but the right hand side evaluated to 616.348267117 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 65.6904096557 ampere but the right hand side evaluated to 616.348267878 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 65.5943350322 ampere but the right hand side evaluated to 616.348268579 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 65.446818975 ampere but the right hand side evaluated to 616.348269331 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 65.2157698202 ampere but the right hand side evaluated to 616.348270344 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 40.8361570363 volt but the right hand side evaluated to 40.044287691 volt (Allowable error: 0.0001%, Actual error: 2%) 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 40.7564335984 volt but the right hand side evaluated to 40.0109034446 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 40.6357802279 volt but the right hand side evaluated to 39.9534916159 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 40.4485541808 volt but the right hand side evaluated to 39.8631072259 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 40.1471961991 volt but the right hand side evaluated to 39.7128058672 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 48.4046054847 ampere but the right hand side evaluated to 462.161071357 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 32.6524167507 volt but the right hand side evaluated to 32.6473151699 volt (Allowable error: 0.0001%, Actual error: 0.016%) 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 48.3769561686 ampere but the right hand side evaluated to 461.90984445 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 32.635764662 volt but the right hand side evaluated to 32.6316113501 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 48.4032696193 ampere but the right hand side evaluated to 462.148922175 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 32.6515981362 volt but the right hand side evaluated to 32.6465415366 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 48.3789750409 ampere but the right hand side evaluated to 461.928187193 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 32.6369846264 volt but the right hand side evaluated to 32.6327619854 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 48.4012400541 ampere but the right hand side evaluated to 462.130475179 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 32.6503712734 volt but the right hand side evaluated to 32.6453838263 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 48.3802998726 ampere but the right hand side evaluated to 461.940228523 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 32.6377916319 volt but the right hand side evaluated to 32.6335238179 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 48.3985076922 ampere but the right hand side evaluated to 462.105654582 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 32.6487408101 volt but the right hand side evaluated to 32.6438475218 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 48.3809307917 ampere but the right hand side evaluated to 461.94596836 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381843217 volt but the right hand side evaluated to 32.6338954013 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 48.3950891412 ampere but the right hand side evaluated to 462.074593438 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 32.6466872742 volt but the right hand side evaluated to 32.6419112618 volt (Allowable error: 0.0001%, Actual error: 0.015%) 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 48.3808902371 ampere but the right hand side evaluated to 461.945587629 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6381402759 volt but the right hand side evaluated to 32.6338518301 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 48.3909804596 ampere but the right hand side evaluated to 462.037257007 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 32.6442080519 volt but the right hand side evaluated to 32.6395726351 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 48.3801406503 ampere but the right hand side evaluated to 461.938777768 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 32.6376887293 volt but the right hand side evaluated to 32.6334260617 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 48.3861590133 ampere but the right hand side evaluated to 461.993457187 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 32.6413157857 volt but the right hand side evaluated to 32.63684638 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 48.3786865577 ampere but the right hand side evaluated to 461.925572636 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 32.6368204727 volt but the right hand side evaluated to 32.6326081888 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 48.3806391398 ampere but the right hand side evaluated to 461.943306814 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 32.6379889347 volt but the right hand side evaluated to 32.633709165 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 48.3765421064 ampere but the right hand side evaluated to 461.906083852 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 32.6355164323 volt but the right hand side evaluated to 32.6313773941 volt (Allowable error: 0.0001%, Actual error: 0.013%) 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 48.3744100341 ampere but the right hand side evaluated to 461.886713061 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 32.6342268759 volt but the right hand side evaluated to 32.6301611382 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 48.3736777936 ampere but the right hand side evaluated to 461.880066457 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 32.6337947002 volt but the right hand side evaluated to 32.6297545135 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 48.3674658021 ampere but the right hand side evaluated to 461.823622437 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 32.6300231787 volt but the right hand side evaluated to 32.6261960798 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 48.3701078413 ampere but the right hand side evaluated to 461.847631584 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 32.6316333738 volt but the right hand side evaluated to 32.6277158 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 48.3597884166 ampere but the right hand side evaluated to 461.753881808 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 32.625380612 volt but the right hand side evaluated to 32.621818164 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 48.3658209518 ampere but the right hand side evaluated to 461.80868118 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 32.6290316027 volt but the right hand side evaluated to 32.6252611351 volt (Allowable error: 0.0001%, Actual error: 0.012%) 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 48.3513870924 ampere but the right hand side evaluated to 461.67755983 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0096%) 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 32.6202766788 volt but the right hand side evaluated to 32.6170034803 volt (Allowable error: 0.0001%, Actual error: 0.01%) 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 48.3608047819 ampere but the right hand side evaluated to 461.763108574 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.011%) 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 32.6259881045 volt but the right hand side evaluated to 32.6223901018 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 48.3422440335 ampere but the right hand side evaluated to 461.594503627 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 32.6147107441 volt but the right hand side evaluated to 32.6117526502 volt (Allowable error: 0.0001%, Actual error: 0.0091%) 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 48.3550541894 ampere but the right hand side evaluated to 461.710864653 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0099%) 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 32.6224935537 volt but the right hand side evaluated to 32.6190933236 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 48.3323582779 ampere but the right hand side evaluated to 461.504697349 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0077%) 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 32.6086660356 volt but the right hand side evaluated to 32.6060484114 volt (Allowable error: 0.0001%, Actual error: 0.008%) 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 48.3485590198 ampere but the right hand side evaluated to 461.651858865 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0093%) 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 32.6185416279 volt but the right hand side evaluated to 32.6153649897 volt (Allowable error: 0.0001%, Actual error: 0.0097%) 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 48.321713747 ampere but the right hand side evaluated to 461.408001264 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0066%) 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 32.6021373133 volt but the right hand side evaluated to 32.5998865834 volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 48.3413111123 ampere but the right hand side evaluated to 461.586016371 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0086%) 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 32.6141226322 volt but the right hand side evaluated to 32.6111956369 volt (Allowable error: 0.0001%, Actual error: 0.009%) 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 48.3102993918 ampere but the right hand side evaluated to 461.304315738 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 32.5951132247 volt but the right hand side evaluated to 32.593256227 volt (Allowable error: 0.0001%, Actual error: 0.0057%) 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 48.3332997978 ampere but the right hand side evaluated to 461.513240995 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0078%) 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 32.6092273737 volt but the right hand side evaluated to 32.6065765032 volt (Allowable error: 0.0001%, Actual error: 0.0081%) 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 48.2980762751 ampere but the right hand side evaluated to 461.193313146 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 32.5876051649 volt but the right hand side evaluated to 32.5861720034 volt (Allowable error: 0.0001%, Actual error: 0.0044%) 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 48.3245050505 ampere but the right hand side evaluated to 461.433358947 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0069%) 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 32.6038529618 volt but the right hand side evaluated to 32.6015059829 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 48.285079839 ampere but the right hand side evaluated to 461.075270939 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 32.5795570403 volt but the right hand side evaluated to 32.5785733117 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 48.3149423442 ampere but the right hand side evaluated to 461.346486363 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0059%) 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 32.5979639618 volt but the right hand side evaluated to 32.5959463323 volt (Allowable error: 0.0001%, Actual error: 0.0062%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 but bound is 0.1460 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 48.271273773 ampere but the right hand side evaluated to 460.949881045 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 32.5709740291 volt but the right hand side evaluated to 32.5704681704 volt (Allowable error: 0.0001%, Actual error: 0.0016%) 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 48.3045571953 ampere but the right hand side evaluated to 461.25216619 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0049%) 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 32.5915838727 volt but the right hand side evaluated to 32.589925686 volt (Allowable error: 0.0001%, Actual error: 0.0051%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.1885 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 0.0315 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 0.0352 but bound is 0.0500 Warning: Constraint [i_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [A]... >= 9.55*i0_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 + Kv_Mission/FlightSeg...] is not tight because the left hand side evaluated to 48.2933599618 ampere but the right hand side evaluated to 461.150470497 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.0037%) Warning: Constraint [v_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40 [V]... >= Kv_Mission/FlightSegment.39/AircraftPerf.39/AircraftDrag.40/MotorPerf.40**-1*omega_Mission/FlightSeg...] is not tight because the left hand side evaluated to 32.5846775692 volt but the right hand side evaluated to 32.5834069402 volt (Allowable error: 0.0001%, Actual error: 0.0039%) Using solver 'mosek' Solving for 9073 variables. Solving took 1.87 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 1.2824 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 882794.0256 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 0.1991 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 0.0328 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 0.0367 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 83.6084089073 ampere but the right hand side evaluated to 779.784421752 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.4%) 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 83.5017269734 ampere but the right hand side evaluated to 779.784421755 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 83.3558110326 ampere but the right hand side evaluated to 779.784421757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 2.1%) 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 83.1310704264 ampere but the right hand side evaluated to 779.78442176 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 82.7771166435 ampere but the right hand side evaluated to 779.784421764 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 38.5658652477 volt but the right hand side evaluated to 37.5903793532 volt (Allowable error: 0.0001%, Actual error: 2.6%) 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 38.4804829835 volt but the right hand side evaluated to 37.5596602597 volt (Allowable error: 0.0001%, Actual error: 2.5%) 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 38.352303314 volt but the right hand side evaluated to 37.5062541098 volt (Allowable error: 0.0001%, Actual error: 2.3%) 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 38.1536775123 volt but the right hand side evaluated to 37.4222334366 volt (Allowable error: 0.0001%, Actual error: 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 37.8404447263 volt but the right hand side evaluated to 37.288010317 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 55.5657294661 ampere but the right hand side evaluated to 530.010860525 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 34.8008471031 volt but the right hand side evaluated to 34.7592625797 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 55.5229512931 ampere but the right hand side evaluated to 529.610507725 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 34.8056775579 volt but the right hand side evaluated to 34.7646195237 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 55.4293437589 ampere but the right hand side evaluated to 528.73317077 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 34.8144007669 volt but the right hand side evaluated to 34.7744114411 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 55.387880013 ampere but the right hand side evaluated to 528.347926319 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 34.8243776931 volt but the right hand side evaluated to 34.7850899168 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 55.280060757 ampere but the right hand side evaluated to 527.337797523 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 34.8361348864 volt but the right hand side evaluated to 34.7981122349 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 55.250492372 ampere but the right hand side evaluated to 527.063149767 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 34.8438227956 volt but the right hand side evaluated to 34.8063079474 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 55.1211535218 ampere but the right hand side evaluated to 525.85376041 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.098%) 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 34.8637181917 volt but the right hand side evaluated to 34.8278886675 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 55.1096352632 ampere but the right hand side evaluated to 525.745652572 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 34.8647837669 volt but the right hand side evaluated to 34.8290772249 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 54.9656195189 ampere but the right hand side evaluated to 524.398646208 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8880257575 volt but the right hand side evaluated to 34.8541802444 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.9640291708 ampere but the right hand side evaluated to 524.383683589 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 34.8881183852 volt but the right hand side evaluated to 34.854287508 volt (Allowable error: 0.0001%, Actual error: 0.097%) 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 54.8052896694 ampere but the right hand side evaluated to 522.898341882 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9147291699 volt but the right hand side evaluated to 34.8829190091 volt (Allowable error: 0.0001%, Actual error: 0.091%) 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 54.816559688 ampere but the right hand side evaluated to 523.00332036 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.087%) 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 34.9117732803 volt but the right hand side evaluated to 34.8797867438 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 54.6413278702 ampere but the right hand side evaluated to 521.363260757 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 34.9429750621 volt but the right hand side evaluated to 34.9132050388 volt (Allowable error: 0.0001%, Actual error: 0.085%) 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 54.6629659499 ampere but the right hand side evaluated to 521.565659532 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 34.9386875469 volt but the right hand side evaluated to 34.9086347883 volt (Allowable error: 0.0001%, Actual error: 0.086%) 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 54.4724435812 ampere but the right hand side evaluated to 519.781464473 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 34.9736241873 volt but the right hand side evaluated to 34.9459257255 volt (Allowable error: 0.0001%, Actual error: 0.079%) 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 54.5066240678 ampere but the right hand side evaluated to 520.101294271 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.077%) 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 34.966463834 volt but the right hand side evaluated to 34.9383236899 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 54.2985169574 ampere but the right hand side evaluated to 518.151644212 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 35.0067189581 volt but the right hand side evaluated to 34.9811130525 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 54.3450909539 ampere but the right hand side evaluated to 518.587769239 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.071%) 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 34.9967693296 volt but the right hand side evaluated to 34.9705804291 volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 54.1187439346 ampere but the right hand side evaluated to 516.466197105 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.064%) 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 35.0427792734 volt but the right hand side evaluated to 35.0192928503 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 54.1771811463 ampere but the right hand side evaluated to 517.013988556 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.066%) 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 35.030391961 volt but the right hand side evaluated to 35.0062092435 volt (Allowable error: 0.0001%, Actual error: 0.069%) 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 53.9316086855 ampere but the right hand side evaluated to 514.710899228 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 35.0828222725 volt but the right hand side evaluated to 35.0615005718 volt (Allowable error: 0.0001%, Actual error: 0.061%) 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 54.0036059342 ampere but the right hand side evaluated to 515.38621133 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.06%) 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 35.0667942944 volt but the right hand side evaluated to 35.04463711 volt (Allowable error: 0.0001%, Actual error: 0.063%) 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 53.7362527867 ampere but the right hand side evaluated to 512.877461401 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.052%) 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 35.1274066463 volt but the right hand side evaluated to 35.10828989 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 53.8228235162 ampere but the right hand side evaluated to 513.689978371 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.055%) 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 35.1070127763 volt but the right hand side evaluated to 35.0869195913 volt (Allowable error: 0.0001%, Actual error: 0.057%) 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 53.532219567 ampere but the right hand side evaluated to 510.961231573 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.046%) 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 35.1768117273 volt but the right hand side evaluated to 35.1599212025 volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 53.634354612 ampere but the right hand side evaluated to 511.920520356 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.049%) 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 35.1513420357 volt but the right hand side evaluated to 35.1333390899 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 53.3163571437 ampere but the right hand side evaluated to 508.932498818 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 35.2332039388 volt but the right hand side evaluated to 35.2185895945 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 53.4360592233 ampere but the right hand side evaluated to 510.057634296 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.043%) 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 35.2012388214 volt but the right hand side evaluated to 35.1853698712 volt (Allowable error: 0.0001%, Actual error: 0.045%) 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 53.0863025383 ampere but the right hand side evaluated to 506.768565338 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 35.2982048172 volt but the right hand side evaluated to 35.2859093893 volt (Allowable error: 0.0001%, Actual error: 0.035%) 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 53.2260967134 ampere but the right hand side evaluated to 508.083694084 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 35.2579542723 volt but the right hand side evaluated to 35.2442613128 volt (Allowable error: 0.0001%, Actual error: 0.039%) 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 52.8379355616 ampere but the right hand side evaluated to 504.430054534 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.027%) 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 35.3746773777 volt but the right hand side evaluated to 35.3647439191 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 53.0016016191 ampere but the right hand side evaluated to 505.97133179 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 35.3234627718 volt but the right hand side evaluated to 35.3119894908 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 52.564032201 ampere but the right hand side evaluated to 501.847996519 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 35.4676825952 volt but the right hand side evaluated to 35.4601585919 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 52.7585501128 ampere but the right hand side evaluated to 503.682031098 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 35.4005617939 volt but the right hand side evaluated to 35.3913478568 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 52.2511821384 ampere but the right hand side evaluated to 498.894235364 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.014%) 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 35.5866744317 volt but the right hand side evaluated to 35.5816052342 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 52.4893884266 ampere but the right hand side evaluated to 501.143678332 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.019%) 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 35.4945466421 volt but the right hand side evaluated to 35.4876363872 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 51.864008574 ampere but the right hand side evaluated to 495.230893642 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 35.756696682 volt but the right hand side evaluated to 35.7541317514 volt (Allowable error: 0.0001%, Actual error: 0.0072%) 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 52.1787663738 ampere but the right hand side evaluated to 498.209734378 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 35.6162404206 volt but the right hand side evaluated to 35.6116863064 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 0.1991 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 0.0328 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 0.0367 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 0.1991 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 0.0328 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 0.0367 but bound is 0.0500 Using solver 'mosek' Solving for 9073 variables. Solving took 2.33 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 1.2351 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 988744.2525 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 0.2106 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 0.0340 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 0.0369 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 99.8053586052 ampere but the right hand side evaluated to 936.51348806 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 99.7125367663 ampere but the right hand side evaluated to 936.513488067 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 99.58659483 ampere but the right hand side evaluated to 936.513488073 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 99.3939660149 ampere but the right hand side evaluated to 936.513488078 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_(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 99.0931269921 ampere but the right hand side evaluated to 936.513488086 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 38.2500451461 volt but the right hand side evaluated to 37.514077418 volt (Allowable error: 0.0001%, Actual error: 2%) 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 38.1813116705 volt but the right hand side evaluated to 37.4858738262 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 38.0772346671 volt but the right hand side evaluated to 37.4367677623 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.9163404395 volt but the right hand side evaluated to 37.3595017064 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.6635835592 volt but the right hand side evaluated to 37.236168113 volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 65.8561545855 ampere but the right hand side evaluated to 627.637728664 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 35.0193479074 volt but the right hand side evaluated to 34.9458879015 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 65.8479245227 ampere but the right hand side evaluated to 627.55804574 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 35.0179742277 volt but the right hand side evaluated to 34.9444437978 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 65.5671103297 ampere but the right hand side evaluated to 624.94478338 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 35.0397531146 volt but the right hand side evaluated to 34.9699437838 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 65.5694993281 ampere but the right hand side evaluated to 624.962357637 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 35.0364693114 volt but the right hand side evaluated to 34.9663573016 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 65.2730564321 ampere but the right hand side evaluated to 622.206544822 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 35.0631698298 volt but the right hand side evaluated to 34.9971872585 volt (Allowable error: 0.0001%, Actual error: 0.19%) 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 65.2858690646 ampere but the right hand side evaluated to 622.319966121 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 35.0580635521 volt but the right hand side evaluated to 34.9915691974 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 64.980217605 ampere but the right hand side evaluated to 619.475345316 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 35.0853612099 volt but the right hand side evaluated to 35.0229720429 volt (Allowable error: 0.0001%, Actual error: 0.18%) 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 65.0009079145 ampere but the right hand side evaluated to 619.663174678 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 35.0800810621 volt but the right hand side evaluated to 35.0171348425 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 64.6876961006 ampere but the right hand side evaluated to 616.743694158 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 35.1068507704 volt but the right hand side evaluated to 35.0478813325 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 64.7128085329 ampere but the right hand side evaluated to 616.976443309 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 35.1036426135 volt but the right hand side evaluated to 35.0442745604 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 64.3850761773 ampere but the right hand side evaluated to 613.922242991 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 35.1344529949 volt but the right hand side evaluated to 35.0793209603 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 64.4225136923 ampere but the right hand side evaluated to 614.26751842 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 35.1280342117 volt but the right hand side evaluated to 35.0722015489 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 64.0817609864 ampere but the right hand side evaluated to 611.090951922 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 35.161841671 volt but the right hand side evaluated to 35.1103917567 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 64.126298255 ampere but the right hand side evaluated to 611.504116748 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 35.1556356207 volt but the right hand side evaluated to 35.1034894654 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 63.7761924212 ampere but the right hand side evaluated to 608.23632914 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 35.1899652107 volt but the right hand side evaluated to 35.14212233 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.826665936 ampere but the right hand side evaluated to 608.707304869 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 35.1846991226 volt but the right hand side evaluated to 35.1362251004 volt (Allowable error: 0.0001%, Actual error: 0.14%) 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 63.4628593642 ampere but the right hand side evaluated to 605.310236342 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 35.222366041 volt but the right hand side evaluated to 35.1783229833 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.5245047317 ampere but the right hand side evaluated to 605.884516658 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 35.2145539565 volt but the right hand side evaluated to 35.169675567 volt (Allowable error: 0.0001%, Actual error: 0.13%) 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 63.1453597894 ampere but the right hand side evaluated to 602.343352273 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 35.2565788154 volt but the right hand side evaluated to 35.2163113039 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 63.2146462713 ampere but the right hand side evaluated to 602.990438731 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 35.2485157316 volt but the right hand side evaluated to 35.2073988513 volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 62.8220491144 ampere but the right hand side evaluated to 599.32088471 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 35.2935930844 volt but the right hand side evaluated to 35.2571326347 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 62.901123139 ampere but the right hand side evaluated to 600.059712172 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 35.2838390549 volt but the right hand side evaluated to 35.2464194714 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 62.4925583136 ampere but the right hand side evaluated to 596.239061427 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 35.3335572874 volt but the right hand side evaluated to 35.3009219843 volt (Allowable error: 0.0001%, Actual error: 0.092%) 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 62.5796605958 ampere but the right hand side evaluated to 597.054395617 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 35.3232404717 volt but the right hand side evaluated to 35.2896293302 volt (Allowable error: 0.0001%, Actual error: 0.095%) 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 62.1578830637 ampere but the right hand side evaluated to 593.10617881 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 35.3757264517 volt but the right hand side evaluated to 35.3468613373 volt (Allowable error: 0.0001%, Actual error: 0.082%) 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 62.2516837251 ampere but the right hand side evaluated to 593.986372493 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 35.365690615 volt but the right hand side evaluated to 35.3358966008 volt (Allowable error: 0.0001%, Actual error: 0.084%) 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 61.806771782 ampere but the right hand side evaluated to 589.821588701 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 35.4273658688 volt but the right hand side evaluated to 35.4026385437 volt (Allowable error: 0.0001%, Actual error: 0.07%) 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 61.9157105134 ampere but the right hand side evaluated to 590.841908963 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 35.4120668701 volt but the right hand side evaluated to 35.3861261917 volt (Allowable error: 0.0001%, Actual error: 0.073%) 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 61.4495280187 ampere but the right hand side evaluated to 586.475748545 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 35.4816325148 volt but the right hand side evaluated to 35.4609243975 volt (Allowable error: 0.0001%, Actual error: 0.058%) 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 61.5712376618 ampere but the right hand side evaluated to 587.615797903 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 35.4626035545 volt but the right hand side evaluated to 35.4405298701 volt (Allowable error: 0.0001%, Actual error: 0.062%) 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 61.0866817702 ampere but the right hand side evaluated to 583.072988575 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 35.5380930857 volt but the right hand side evaluated to 35.5212382847 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 61.2164194433 ampere but the right hand side evaluated to 584.290705504 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.048%) 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 35.5184103521 volt but the right hand side evaluated to 35.5002380338 volt (Allowable error: 0.0001%, Actual error: 0.051%) 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 60.700552085 ampere but the right hand side evaluated to 579.452985745 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 35.608176318 volt but the right hand side evaluated to 35.5955518035 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 60.8482167522 ampere but the right hand side evaluated to 580.838213566 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 35.5813704419 volt but the right hand side evaluated to 35.5671756923 volt (Allowable error: 0.0001%, Actual error: 0.04%) 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 60.300708967 ampere but the right hand side evaluated to 575.699965461 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.022%) 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 35.6855327794 volt but the right hand side evaluated to 35.6770679251 volt (Allowable error: 0.0001%, Actual error: 0.024%) 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 60.4639007707 ampere but the right hand side evaluated to 577.232164565 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 35.6531577824 volt but the right hand side evaluated to 35.6430158767 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 59.8791591274 ampere but the right hand side evaluated to 571.739248605 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 35.7752524698 volt but the right hand side evaluated to 35.7709876352 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 60.0608422653 ampere but the right hand side evaluated to 573.446746715 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 35.7353737506 volt but the right hand side evaluated to 35.7293207916 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 0.2106 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 0.0340 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 0.0369 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 59.6316150477 ampere but the right hand side evaluated to 569.411419133 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 35.83271024 volt but the right hand side evaluated to 35.8308144951 volt (Allowable error: 0.0001%, Actual error: 0.0053%) Using solver 'mosek' Solving for 4713 variables. Solving took 1.01 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 1.2058 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 1064456.8431 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 0.2186 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 0.0349 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 0.0382 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 111.917770052 ampere but the right hand side evaluated to 1056.06638259 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.846508662 ampere but the right hand side evaluated to 1056.0663826 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750496698 ampere but the right hand side evaluated to 1056.06638261 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604583491 ampere but the right hand side evaluated to 1056.06638263 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378520141 ampere but the right hand side evaluated to 1056.06638264 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2100050587 volt but the right hand side evaluated to 37.703700589 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552266825 volt but the right hand side evaluated to 37.676874408 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0707683706 volt but the right hand side evaluated to 37.6300619441 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401395681 volt but the right hand side evaluated to 37.5563494017 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350514783 volt but the right hand side evaluated to 37.438674283 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3928809075 ampere but the right hand side evaluated to 699.259437341 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 35.2475796756 volt but the right hand side evaluated to 35.1620021793 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 73.0287800896 ampere but the right hand side evaluated to 695.874661344 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 35.2657860571 volt but the right hand side evaluated to 35.1847556766 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6668707247 ampere but the right hand side evaluated to 692.503909994 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 35.2825360344 volt but the right hand side evaluated to 35.2057286888 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3030178084 ampere but the right hand side evaluated to 689.114223932 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 35.3004423704 volt but the right hand side evaluated to 35.2278760326 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9368569251 ampere but the right hand side evaluated to 685.702214533 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 35.319619583 volt but the right hand side evaluated to 35.2513177671 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 71.5698251276 ampere but the right hand side evaluated to 682.279116183 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 35.339012059 volt but the right hand side evaluated to 35.2748651266 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 71.1962375207 ampere but the right hand side evaluated to 678.798172587 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 35.3621860732 volt but the right hand side evaluated to 35.3024907896 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211296589 ampere but the right hand side evaluated to 675.299841866 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 35.3857488327 volt but the right hand side evaluated to 35.3303922636 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4425563445 ampere but the right hand side evaluated to 671.767772507 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 35.4108388785 volt but the right hand side evaluated to 35.3598286042 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 70.0657091443 ampere but the right hand side evaluated to 668.244857313 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 35.4340101959 volt but the right hand side evaluated to 35.3869854277 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 69.6718387141 ampere but the right hand side evaluated to 664.57383587 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 35.4671381102 volt but the right hand side evaluated to 35.4249433772 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 69.2796432549 ampere but the right hand side evaluated to 660.910358539 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 35.498126478 volt but the right hand side evaluated to 35.4603417137 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8779735265 ampere but the right hand side evaluated to 657.159927166 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 35.533956436 volt but the right hand side evaluated to 35.5008295264 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4704569338 ampere but the right hand side evaluated to 653.352346267 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.5721823924 volt but the right hand side evaluated to 35.5436931336 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.056541243 ampere but the right hand side evaluated to 649.482187165 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/Aircraf.tDrag.138/MotorPerf.138**-1*omega_Mission.3/F...] is not tight because the left hand side evaluated to 35.6130215752 volt but the right hand side evaluated to 35.5891420148 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.634264213 ampere but the right hand side evaluated to 645.531677118 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 35.6575716444 volt but the right hand side evaluated to 35.6383309899 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.2007894609 ampere but the right hand side evaluated to 641.474965924 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 35.7074599538 volt but the right hand side evaluated to 35.6929628154 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 66.7560033352 ampere but the right hand side evaluated to 637.30952997 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 35.7625903813 volt but the right hand side evaluated to 35.7528622718 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 66.2964767541 ampere but the right hand side evaluated to 633.003334149 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 35.8249158544 volt but the right hand side evaluated to 35.8200292515 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission.3/Aircraft.3/Wing.3/Planform.11 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 571 variables. Solving took 0.199 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 1.2058 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 1064456.8406 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 0.2186 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 0.0349 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 0.0382 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 111.920982833 ampere but the right hand side evaluated to 1056.0663751 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.849323672 ampere but the right hand side evaluated to 1056.06637512 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.752850386 ampere but the right hand side evaluated to 1056.06637514 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.606364764 ampere but the right hand side evaluated to 1056.06637516 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.379914674 ampere but the right hand side evaluated to 1056.06637518 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2086428026 volt but the right hand side evaluated to 37.7038065545 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1536792396 volt but the right hand side evaluated to 37.6769672477 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0690626248 volt but the right hand side evaluated to 37.6301395605 volt (Allowable error: 0.0001%, Actual error: 1.2%) Warning: Constra.int [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 37.9383538985 volt but the right hand side evaluated to 37.5564081288 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7337082178 volt but the right hand side evaluated to 37.4387202459 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 571 variables. Solving took 0.164 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 1.2058 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 1064456.8406 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 0.2186 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 0.0349 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 0.0382 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 111.920983071 ampere but the right hand side evaluated to 1056.06637509 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.849323864 ampere but the right hand side evaluated to 1056.06637511 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.752850524 ampere but the right hand side evaluated to 1056.06637513 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.606364832 ampere but the right hand side evaluated to 1056.06637515 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.379914696 ampere but. the right hand side evaluated to 1056.06637517 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.208642739 volt but the right hand side evaluated to 37.7038065622 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1536791587 volt but the right hand side evaluated to 37.6769672538 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.0690625246 volt but the right hand side evaluated to 37.6301395648 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9383537792 volt but the right hand side evaluated to 37.5564081308 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7337081204 volt but the right hand side evaluated to 37.4387202465 volt (Allowable error: 0.0001%, Actual error: 0.79%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Using solver 'mosek' Solving for 4713 variables. Solving took 1.16 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 1.2058 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 1064456.8435 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 0.2186 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 0.0349 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 0.0382 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 111.91781048 ampere but the right hand side evaluated to 1056.06638257 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.846541075 ampere but the right hand side evaluated to 1056.06638258 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750518933 ampere but the right hand side evaluated to 1056.0663826 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604592233 ampere but the right hand side evaluated to 1056.06638261 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378511001 ampere but the right hand side evaluated to 1056.06638263 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2100217709 volt but the right hand side evaluated to 37.7037019448 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552398257 volt but the right hand side evaluated to 37.6768754992 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.070777112 volt but the right hand side evaluated to 37.6300626995 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.940142573 volt but the right hand side evaluated to 37.5563497118 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350478144 volt but the right hand side evaluated to 37.4386740031 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3931399317 ampere but the right hand side evaluated to 699.262943383 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 35.2475644303 volt but the right hand side evaluated to 35.1620428012 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 73.0289049949 ampere but the right hand side evaluated to 695.876969183 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 35.2658444919 volt but the right hand side evaluated to 35.1848744094 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6669887713 ampere but the right hand side evaluated to 692.506036695 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 35.2825856688 volt but the right hand side evaluated to 35.2058326465 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3031318237 ampere but the right hand side evaluated to 689.116198282 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 35.3004819325 volt but the right hand side evaluated to 35.2279639881 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9369637891 ampere but the right hand side evaluated to 685.704017571 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 35.3196516875 volt but the right hand side evaluated to 35.2513928635 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 71.5699950948 ampere but the right hand side evaluated to 682.281328939 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 35.3389920492 volt but the right hand side evaluated to 35.274877826 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 71.1963081385 ampere but the right hand side evaluated to 678.799470934 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 35.3622191785 volt but the right hand side evaluated to 35.3025585123 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211717363 ampere but the right hand side evaluated to 675.300809206 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 35.3857899763 volt but the right hand side evaluated to 35.3304649206 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4426759546 ampere but the right hand side evaluated to 671.769293711 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 35.410820512 volt but the right hand side evaluated to 35.3598315971 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 70.0648746622 ampere but the right hand side evaluated to 668.23833607 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 35.4345945362 volt but the right hand side evaluated to 35.387650194 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 69.6718343987 ampere but the right hand side evaluated to 664.574163311 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 35.4671815905 volt but the right hand side evaluated to 35.4250077244 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 69.2794508201 ampere but the right hand side evaluated to 660.909022271 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 35.4982818287 volt but the right hand side evaluated to 35.4605254377 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8780413361 ampere but the right hand side evaluated to 657.160731274 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 35.533939118 volt but the right hand side evaluated to 35.500821244 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4705011768 ampere but the right hand side evaluated to 653.352894171 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.57217367 volt but the right hand side evaluated to 35.5436916813 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.0565747141 ampere but the right hand side evaluated to 649.482595386 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 35.6130142097 volt but the right hand side evaluated to 35.5891398158 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.6342936614 ampere but the right hand side evaluated to 645.53201139 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 35.6575622376 volt but the right hand side evaluated to 35.6383246967 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.200804915 ampere but the right hand side evaluated to 641.475147247 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 35.707455678 volt but the right hand side evaluated to 35.6929605256 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 66.7560125128 ampere but the right hand side evaluated to 637.309632008 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 35.7625871689 volt but the right hand side evaluated to 35.7528599122 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 66.296478799 ampere but the right hand side evaluated to 633.00335761 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 35.8249152384 volt but the right hand side evaluated to 35.8200288701 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 7.42 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 1.2115 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 1024485.2866 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 0.2113 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 0.0257 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 0.0393 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 103.180116482 ampere but the right hand side evaluated to 968.100177777 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 103.085445972 ampere but the right hand side evaluated to 968.100177795 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 102.957161685 ampere but the right hand side evaluated to 968.100177809 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 102.761207112 ampere but the right hand side evaluated to 968.100177828 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 102.455482094 ampere but the right hand side evaluated to 968.100177853 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 37.9242671602 volt but the right hand side evaluated to 37.1871423443 volt (Allowable error: 0.0001%, Actual error: 2%) 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 37.8575886955 volt but the right hand side evaluated to 37.1603769096 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 37.7565345226 volt but the right hand side evaluated to 37.1133868754 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.6004436505 volt but the right hand side evaluated to 37.0394318447 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.3554068199 volt but the right hand side evaluated to 36.9213677198 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 68.3453815901 ampere but the right hand side evaluated to 651.14739435 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 34.6911556149 volt but the right hand side evaluated to 34.6060531533 volt (Allowable error: 0.0001%, Actual error: 0.25%) 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 67.9970156316 ampere but the right hand side evaluated to 647.9089882 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 34.7124926171 volt but the right hand side evaluated to 34.6319596916 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 67.6517504928 ampere but the right hand side evaluated to 644.692671896 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 34.7317735201 volt but the right hand side evaluated to 34.6554359524 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 67.3042186804 ampere but the right hand side evaluated to 641.454324 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 34.7524589839 volt but the right hand side evaluated to 34.6803337967 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 66.9539902348 ampere but the right hand side evaluated to 638.189956726 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 34.7747171185 volt but the right hand side evaluated to 34.7068286708 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 66.6031147856 ampere but the right hand side evaluated to 634.916343404 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 34.7970876937 volt but the right hand side evaluated to 34.7333033322 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 66.2438495214 ampere but the right hand side evaluated to 631.568038086 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 34.8245376922 volt but the right hand side evaluated to 34.7652050761 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 65.8831989404 ampere but the right hand side evaluated to 628.20331953 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 34.8523536382 volt but the right hand side evaluated to 34.7973357593 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 65.5190194381 ampere but the right hand side evaluated to 624.803761817 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 34.8818299401 volt but the right hand side evaluated to 34.8311054462 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 65.1525091144 ampere but the right hand side evaluated to 621.379256307 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 34.9120773269 volt but the right hand side evaluated to 34.8655353718 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 64.7735918552 ampere but the right hand side evaluated to 617.842580976 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 34.9495232735 volt but the right hand side evaluated to 34.9075775205 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 64.3922722059 ampere but the right hand side evaluated to 614.279017306 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 34.9875505985 volt but the right hand side evaluated to 34.9500212955 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 64.0015324089 ampere but the right hand side evaluated to 610.627132897 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 35.0305878523 volt but the right hand side evaluated to 34.9976240965 volt (Allowable error: 0.0001%, Actual error: 0.094%) 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 63.6023455472 ampere but the right hand side evaluated to 606.894355658 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 35.0778803556 volt but the right hand side evaluated to 35.0495250527 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 63.1951815953 ampere but the right hand side evaluated to 603.083898309 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 35.1290044622 volt but the right hand side evaluated to 35.1052265959 volt (Allowable error: 0.0001%, Actual error: 0.068%) 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 62.7772999441 ampere but the right hand side evaluated to 599.170553889 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.051%) 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/Fli.gh...] is not tight because the left hand side evaluated to 35.1856009352 volt but the right hand side evaluated to 35.1664300671 volt (Allowable error: 0.0001%, Actual error: 0.055%) 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 62.3445853958 ampere but the right hand side evaluated to 595.116277396 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 35.2501808617 volt but the right hand side evaluated to 35.2357279606 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 61.8960720153 ampere but the right hand side evaluated to 590.910400962 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 35.3232153463 volt but the right hand side evaluated to 35.3135091173 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 61.4259305284 ampere but the right hand side evaluated to 586.497970584 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 35.4082784509 volt but the right hand side evaluated to 35.4033990865 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 0.2113 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 0.0257 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 0.0393 but bound is 0.0500 Using solver 'mosek_cli' Solving for 4713 variables. Solving took 1.08 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 1.2058 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 1064461.9306 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 0.2186 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 0.0349 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 0.0382 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 111.91772465 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 111.84645576 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 111.750532658 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1%) 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 111.604570119 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.92%) 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 111.378465399 ampere but the right hand side evaluated to 1056.06637802 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.71%) 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 38.2099900097 volt but the right hand side evaluated to 37.7037124356 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.1552361519 volt but the right hand side evaluated to 37.6768818679 volt (Allowable error: 0.0001%, Actual error: 1.3%) 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 38.070777763 volt but the right hand side evaluated to 37.6300725084 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 37.9401531069 volt but the right hand side evaluated to 37.5563550079 volt (Allowable error: 0.0001%, Actual error: 1%) 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 37.7350360091 volt but the right hand side evaluated to 37.4386798186 volt (Allowable error: 0.0001%, Actual error: 0.79%) 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 73.3928852703 ampere but the right hand side evaluated to 699.259252504 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 35.2475844264 volt but the right hand side evaluated to 35.1620175348 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 73.0288084791 ampere but the right hand side evaluated to 695.875002379 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 35.2657768732 volt but the right hand side evaluated to 35.1847586308 volt (Allowable error: 0.0001%, Actual error: 0.23%) 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 72.6669010809 ampere but the right hand side evaluated to 692.503656937 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 35.2825320963 volt but the right hand side evaluated to 35.2057381181 volt (Allowable error: 0.0001%, Actual error: 0.22%) 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 72.3030273248 ampere but the right hand side evaluated to 689.114181043 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 35.3004601759 volt but the right hand side evaluated to 35.2278680724 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 71.9368751189 ampere but the right hand side evaluated to 685.702542038 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 35.3196335309 volt but the right hand side evaluated to 35.2513063048 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 71.5698574506 ampere but the right hand side evaluated to 682.278868389 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 35.3389939944 volt but the right hand side evaluated to 35.2748531353 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 71.196239428 ampere but the right hand side evaluated to 678.798399874 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 35.3621839799 volt but the right hand side evaluated to 35.302504444 volt (Allowable error: 0.0001%, Actual error: 0.17%) 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 70.8211014944 ampere but the right hand side evaluated to 675.299571033 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 35.3857430387 volt but the right hand side evaluated to 35.3303851139 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 70.4425863487 ampere but the right hand side evaluated to 671.76780333 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 35.4108404265 volt but the right hand side evaluated to 35.3598222095 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 70.0656738448 ampere but the right hand side evaluated to 668.244506754 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.12%) 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 35.4340066907 volt but the right hand side evaluated to 35.3869840023 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 69.6718247479 ampere but the right hand side evaluated to 664.573718666 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 35.4671529804 volt but the right hand side evaluated to 35.4249283144 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 69.2796352934 ampere but the right hand side evaluated to 660.910267925 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 35.4981293242 volt but the right hand side evaluated to 35.4603518177 volt (Allowable error: 0.0001%, Actual error: 0.11%) 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 68.8779432657 ampere but the right hand side evaluated to 657.159687095 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 35.5339650128 volt but the right hand side evaluated to 35.5008151603 volt (Allowable error: 0.0001%, Actual error: 0.093%) 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 68.4704318325 ampere but the right hand side evaluated to 653.35251579 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 0.075%) 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 35.5721845645 volt but the right hand side evaluated to 35.5437029519 volt (Allowable error: 0.0001%, Actual error: 0.08%) 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 68.0565515503 ampere but the right hand side evaluated to 649.482206845 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 35.6130092687 volt but the right hand side evaluated to 35.5891434405 volt (Allowable error: 0.0001%, Actual error: 0.067%) 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 67.6342830362 ampere but the right hand side evaluated to 645.531584282 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 35.6575890221 volt but the right hand side evaluated to 35.6383203702 volt (Allowable error: 0.0001%, Actual error: 0.054%) 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 67.2007897707 ampere but the right hand side evaluated to 641.475009679 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 35.7074731924 volt but the right hand side evaluated to 35.6929701349 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 66.7559879251 ampere but the right hand side evaluated to 637.309625955 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 35.7625765899 volt but the right hand side evaluated to 35.7528572379 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 66.2964930089 ampere but the right hand side evaluated to 633.003278394 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 35.8249292918 volt but the right hand side evaluated to 35.8200255905 volt (Allowable error: 0.0001%, Actual error: 0.014%) Warning: Variable tau_Mission/Aircraft/Wing/Planform.2 could cause inaccurate result because it is above upper bound. Solution is 0.2186 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 0.0349 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 0.0382 but bound is 0.0500 Beginning signomial solve. Solving took 4 GP solves and 9.19 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 1.2115 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 1024484.3799 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 0.2113 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 0.0257 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 0.0393 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 103.179893125 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.8%) 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 103.085320531 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 102.957059166 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.6%) 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 102.761215428 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.4%) 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 102.455545289 ampere but the right hand side evaluated to 968.100504122 meter * newton * revolutions_per_minute / volt (Allowable error: 0.0001%, Actual error: 1.1%) 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 37.9241836643 volt but the right hand side evaluated to 37.1871409632 volt (Allowable error: 0.0001%, Actual error: 2%) 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 37.8575336611 volt but the right hand side evaluated to 37.1603807992 volt (Allowable error: 0.0001%, Actual error: 1.9%) 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 37.7565133544 volt but the right hand side evaluated to 37.1133694409 volt (Allowable error: 0.0001%, Actual error: 1.7%) 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 37.6004493078 volt but the right hand side evaluated to 37.0394414661 volt (Allowable error: 0.0001%, Actual error: 1.5%) 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 37.3554568011 volt but the right hand side evaluated to 36.9213822508 volt (Allowable error: 0.0001%, Actual error: 1.2%) 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 68.3448354525 ampere but the right hand side evaluated to 651.139634182 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 34.6911634881 volt but the right hand side evaluated to 34.6059019965 volt (Allowable error: 0.0001%, Actual error: 0.25%) 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 67.9968241222 ampere but the right hand side evaluated to 647.904303437 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 34.7122968411 volt but the right hand side evaluated to 34.6316097356 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 67.6515319775 ampere but the right hand side evaluated to 644.688590865 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 34.7316022445 volt but the right hand side evaluated to 34.6551154539 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 67.3040221936 ampere but the right hand side evaluated to 641.450471552 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 34.7523084493 volt but the right hand side evaluated to 34.6800462207 volt (Allowable error: 0.0001%, Actual error: 0.21%) 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 66.9538114289 ampere but the right hand side evaluated to 638.186325829 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 34.7745918201 volt but the right hand side evaluated to 34.7065860277 volt (Allowable error: 0.0001%, Actual error: 0.2%) 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 66.6027587926 ampere but the right hand side evaluated to 634.911569203 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 34.797098261 volt but the right hand side evaluated to 34.7332078372 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 66.2437419982 ampere but the right hand side evaluated to 631.565945243 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 34.824389883 volt but the right hand side evaluated to 34.7649868307 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 65.8831685544 ampere but the right hand side evaluated to 628.201774725 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 34.8521908372 volt but the right hand side evaluated to 34.7970991815 volt (Allowable error: 0.0001%, Actual error: 0.16%) 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 65.5187918522 ampere but the right hand side evaluated to 624.800974192 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 34.8818277933 volt but the right hand side evaluated to 34.8310402225 volt (Allowable error: 0.0001%, Actual error: 0.15%) 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 65.1548014993 ampere but the right hand side evaluated to 621.397955272 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 34.9104775331 volt but the right hand side evaluated to 34.8637502062 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 64.7737222319 ampere but the right hand side evaluated to 617.842352999 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 34.9493545256 volt but the right hand side evaluated to 34.9073593924 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 64.3928756218 ampere but the right hand side evaluated to 614.283468853 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 34.9870852312 volt but the right hand side evaluated to 34.9494971368 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 64.0014026804 ampere but the right hand side evaluated to 610.625693746 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 35.0306012177 volt but the right hand side evaluated to 34.9976232036 volt (Allowable error: 0.0001%, Actual error: 0.094%) 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 63.6022597261 ampere but the right hand side evaluated to 606.893206384 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 35.0778893875 volt but the right hand side evaluated to 35.0494976305 volt (Allowable error: 0.0001%, Actual error: 0.081%) 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 63.195114756 ampere but the right hand side evaluated to 603.083311633 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 evaluate. ---------------------------------------------------------------------- Ran 6 tests in 206.522s OK Generating XML reports... d to 35.1289999939 volt but the right hand side evaluated to 35.1051987827 volt (Allowable error: 0.0001%, Actual error: 0.068%) 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 62.7772659018 ampere but the right hand side evaluated to 599.170103847 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 35.1856032373 volt but the right hand side evaluated to 35.1664497638 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 62.3445338826 ampere but the right hand side evaluated to 595.115806014 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 35.2501928442 volt but the right hand side evaluated to 35.2357400308 volt (Allowable error: 0.0001%, Actual error: 0.041%) 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 61.8960893007 ampere but the right hand side evaluated to 590.910211685 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 35.3232009941 volt but the right hand side evaluated to 35.3135051811 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 61.4259263938 ampere but the right hand side evaluated to 586.497990346 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 35.4082909378 volt but the right hand side evaluated to 35.4033923764 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 0.2113 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 0.0257 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 0.0393 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-MK3Wrv 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-EGTo6x/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-MiK_D9/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 6.383s 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 0.0749 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.242 seconds. Using solver 'mosek' Solving for 8 variables. Solving took 0.0224 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.0234 seconds. Using solver 'mosek' Solving for 24 variables. Solving took 0.0241 seconds. Using solver 'mosek_cli' Solving for 8 variables. Solving took 0.228 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.229 seconds. Using solver 'mosek_cli' Solving for 24 variables. Solving took 0.233 seconds. Using solver 'mosek' Solving for 13 variables. Solving took 0.0311 seconds. Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.231 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 1884891.4063 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1656770.2552 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 1.663s 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