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Skipping 33 KB.. Full LogRequirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.23.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-fgpij_ Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.0) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->gpfit==0.1) (2018.0.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->gpfit==0.1) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-ovcoll\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpfit Successfully installed gpfit-0.1 Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gassolar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.23.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.2.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->gassolar==0.0.0.0) (2018.0.0) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas->gassolar==0.0.0.0) (1.11.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->gassolar==0.0.0.0) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-yflnp2\wheels\08\33\b8\d36cec4e8239569444cd725d0dbfe83a0cfc534951775e5535 Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gassolar Successfully installed gassolar-0.0.0.0 adding test for 'gassolar/gas/gas.py' adding test for 'gassolar/solar/solar.py' Using solver 'mosek' Solving for 592 variables. Solving took 1.01 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 3.09 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 0.195 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 7.8 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 8.31 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 3.47 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 4.54 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 6.59 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 Running tests... ---------------------------------------------------------------------- ..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) .. ---------------------------------------------------------------------- Ran 4 tests in 70.804s OK Generating XML reports... Cloning into 'jho'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.23.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-h7tugm Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.0) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->gpfit==0.1) (2018.0.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->gpfit==0.1) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-2dvjbk\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'model/jho.py' adding test for 'model/print_perf.py' Beginning signomial solve. Allowing negative dual variable(s) as small as -5.222081447819882e-14. Allowing negative dual variable(s) as small as -7.84905994366536e-14. Allowing negative dual variable(s) as small as -1.5087106911004788e-13. Allowing negative dual variable(s) as small as -1.4810505252760287e-13. Solving took 4 GP solves and 22.3 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.297541919024873e-14. Allowing negative dual variable(s) as small as -7.555978412399078e-14. Allowing negative dual variable(s) as small as -1.5259278215995487e-13. Allowing negative dual variable(s) as small as -1.4901101186293175e-13. Solving took 4 GP solves and 17.7 seconds. Allowing negative dual variable(s) as small as -5.188141583012396e-13. Allowing negative dual variable(s) as small as -1.4275178261691224e-12. Allowing negative dual variable(s) as small as -4.4540933441528097e-13. Allowing negative dual variable(s) as small as -4.4316807168431893e-13. Allowing negative dual variable(s) as small as -1.2961689013768485e-12. Allowing negative dual variable(s) as small as -1.0913420774721905e-12. Allowing negative dual variable(s) as small as -1.0920474594056095e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 Wing span [ft] = 24.00 Aicraft length [ft] = 12.90 Aspect ratio = 25.60 mean aerodynamic chord [ft] = 0.9722 root chord [ft] = 1.250 speed for best rate of climb [m/s]: Vy = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -2.469812548921979e-15. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.541623049278133e-14. Allowing negative dual variable(s) as small as -5.695972194941673e-12. Allowing negative dual variable(s) as small as -2.0878956970575863e-11. Allowing negative dual variable(s) as small as -2.088093075838094e-11. Solving took 4 GP solves and 5.5 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.2 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.182104745315996e-13. Allowing negative dual variable(s) as small as -1.4288448896282446e-12. Allowing negative dual variable(s) as small as -4.433259315206328e-13. Allowing negative dual variable(s) as small as -4.445784018702881e-13. Allowing negative dual variable(s) as small as -1.296617110554954e-12. Allowing negative dual variable(s) as small as -1.0918680239460632e-12. Allowing negative dual variable(s) as small as -1.0902314207666963e-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 -2.487555273952732e-14. Allowing negative dual variable(s) as small as -5.695872395243426e-12. Allowing negative dual variable(s) as small as -2.0878999602141145e-11. Allowing negative dual variable(s) as small as -2.0880952599363714e-11. Solving took 4 GP solves and 9.82 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 3.32 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Running tests... ---------------------------------------------------------------------- .... ---------------------------------------------------------------------- Ran 4 tests in 132.705s OK Generating XML reports... Cloning into 'turbofan'... Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\turbofan Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.1.0) Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-yexjjv\wheels\e5\cb\a8\3b11c975e79b3f632de8c1b88ce438a834a6b07b3850d6b107 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: turbofan Successfully installed turbofan-0.0.0.0 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 24184.7528322 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 26232.8485075 newton but the right hand side evaluated to 26232.36 newton (Allowable error: 0.0001%, Actual error: 0.0019%) Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 3.108s OK Generating XML reports... Cloning into 'SPaircraft'... 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Collecting git+https://github.com/hoburg/turbofan.git Cloning https://github.com/hoburg/turbofan.git to c:\users\jenkins\appdata\local\temp\pip-req-build-tsbrvr Requirement already satisfied (use --upgrade to upgrade): turbofan==0.0.0.0 from git+https://github.com/hoburg/turbofan.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from turbofan==0.0.0.0) (1.1.0) Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-b6r_yc\wheels\49\e6\3a\5de0d21c0f148404ea8d883f76e050c82d4e9a0e6f59ce69a5 Successfully built turbofan grin 1.2.1 requires argparse>=1.1, which is not installed. adding test for 'SP_aircraft.py' Beginning signomial solve. Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Windows/64-X86 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1016 Eliminator terminated. Eliminator started. Total number of eliminations : 1025 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1025 Lin. dep. - tries : 1 time : 0.01 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 826 Optimizer - Cones : 0 Optimizer - Scalar variables : 3575 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.67e+004 after factor : 1.69e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.291593405e+005 2.000000000e+000 1.0e+000 0.06 1 1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.269655162e+005 3.700395480e+000 4.8e-001 0.13 2 3.9e+002 5.0e+002 2.2e+004 -9.36e-001 -1.198083099e+005 1.153971197e+001 1.7e-001 0.16 3 2.8e+002 3.7e+002 1.6e+004 -8.23e-001 -1.159038545e+005 8.917911751e+001 1.2e-001 0.20 4 2.8e+002 3.6e+002 1.6e+004 -7.55e-001 -1.129120590e+005 2.532205882e+003 1.2e-001 0.23 5 6.9e+001 9.1e+001 3.9e+003 -7.46e-001 -7.042317639e+004 1.170731339e+004 3.1e-002 0.27 6 3.1e+001 4.1e+001 1.8e+003 -1.38e-001 -4.093680277e+004 1.097631330e+004 1.4e-002 0.30 7 1.6e+001 2.1e+001 9.1e+002 3.74e-001 -2.381570953e+004 6.691140297e+003 7.1e-003 0.31 8 7.3e+000 9.5e+000 4.1e+002 6.72e-001 -1.127653330e+004 3.750639855e+003 3.3e-003 0.33 9 3.4e+000 4.4e+000 1.9e+002 8.76e-001 -5.047557905e+003 2.145533564e+003 1.5e-003 0.36 10 1.7e+000 2.2e+000 9.8e+001 9.57e-001 -2.254111634e+003 1.439335762e+003 7.7e-004 0.37 11 6.4e-001 8.4e-001 3.7e+001 9.85e-001 -6.385796056e+002 7.706340105e+002 2.9e-004 0.39 12 5.5e-001 7.6e-001 3.2e+001 9.81e-001 -5.013262073e+002 7.168373519e+002 2.5e-004 0.41 13 3.9e-001 9.4e-001 2.3e+001 9.74e-001 -2.540202679e+002 6.153446061e+002 1.8e-004 0.44 14 2.1e-001 6.0e-001 1.2e+001 9.86e-001 2.138010426e+001 4.968168260e+002 9.8e-005 0.45 15 6.4e-002 2.4e-001 3.8e+000 1.00e+000 2.550914158e+002 4.006034777e+002 3.0e-005 0.47 16 2.0e-002 1.4e-001 1.2e+000 1.00e+000 3.243614726e+002 3.710224804e+002 9.9e-006 0.50 17 4.6e-003 1.5e-001 2.8e-001 1.00e+000 3.495900434e+002 3.605469978e+002 2.4e-006 0.52 18 2.7e-003 1.2e-001 1.7e-001 1.00e+000 3.526439438e+002 3.591745038e+002 1.4e-006 0.53 19 6.1e-004 1.3e-001 3.9e-002 9.95e-001 3.562634844e+002 3.577655674e+002 3.3e-007 0.55 20 2.3e-004 1.0e-001 1.5e-002 9.96e-001 3.569347900e+002 3.575083937e+002 1.3e-007 0.56 21 1.1e-004 8.0e-002 7.0e-003 1.00e+000 3.571540631e+002 3.574256285e+002 5.9e-008 0.59 22 9.9e-005 7.3e-002 6.3e-003 1.00e+000 3.571735322e+002 3.574179282e+002 5.3e-008 0.61 23 8.9e-005 6.6e-002 5.7e-003 9.99e-001 3.571910260e+002 3.574109857e+002 4.8e-008 0.62 24 8.0e-005 6.0e-002 5.1e-003 1.00e+000 3.572067759e+002 3.574047494e+002 4.3e-008 0.64 25 7.2e-005 5.5e-002 4.6e-003 1.00e+000 3.572209513e+002 3.573991334e+002 3.9e-008 0.66 26 6.5e-005 5.0e-002 4.2e-003 1.00e+000 3.572337075e+002 3.573940737e+002 3.5e-008 0.69 27 5.9e-005 4.5e-002 3.7e-003 1.00e+000 3.572451862e+002 3.573895160e+002 3.2e-008 0.70 28 5.3e-005 4.2e-002 3.4e-003 1.00e+000 3.572555163e+002 3.573854124e+002 2.8e-008 0.72 29 4.7e-005 3.8e-002 3.0e-003 1.00e+000 3.572648135e+002 3.573817190e+002 2.6e-008 0.73 30 4.3e-005 3.5e-002 2.7e-003 1.00e+000 3.572731816e+002 3.573783955e+002 2.3e-008 0.76 31 3.8e-005 3.2e-002 2.5e-003 1.00e+000 3.572807140e+002 3.573754055e+002 2.1e-008 0.80 32 3.5e-005 3.0e-002 2.2e-003 1.00e+000 3.572874942e+002 3.573727158e+002 1.9e-008 0.84 33 3.1e-005 2.7e-002 2.0e-003 1.00e+000 3.572935975e+002 3.573702962e+002 1.7e-008 0.87 34 2.8e-005 2.5e-002 1.8e-003 1.00e+000 3.572990917e+002 3.573681199e+002 1.5e-008 0.94 35 2.5e-005 2.3e-002 1.6e-003 1.00e+000 3.573040375e+002 3.573661624e+002 1.4e-008 0.98 36 2.3e-005 2.2e-002 1.4e-003 1.00e+000 3.573084897e+002 3.573644018e+002 1.2e-008 1.01 37 2.0e-005 2.0e-002 1.3e-003 1.00e+000 3.573124975e+002 3.573628181e+002 1.1e-008 1.04 38 1.8e-005 1.9e-002 1.2e-003 1.00e+000 3.573161054e+002 3.573613937e+002 9.9e-009 1.09 39 1.7e-005 1.8e-002 1.1e-003 1.00e+000 3.573193532e+002 3.573601125e+002 8.9e-009 1.12 40 1.5e-005 1.7e-002 9.5e-004 1.00e+000 3.573222768e+002 3.573589600e+002 8.0e-009 1.15 41 1.3e-005 1.6e-002 8.6e-004 1.00e+000 3.573249085e+002 3.573579234e+002 7.2e-009 1.20 42 1.2e-005 1.5e-002 7.7e-004 1.00e+000 3.573272776e+002 3.573569909e+002 6.5e-009 1.23 43 1.1e-005 1.4e-002 6.9e-004 1.00e+000 3.573294101e+002 3.573561520e+002 5.8e-009 1.26 44 9.8e-006 1.3e-002 6.2e-004 1.00e+000 3.573313297e+002 3.573553974e+002 5.3e-009 1.28 45 8.8e-006 1.3e-002 5.6e-004 1.00e+000 3.573330576e+002 3.573547186e+002 4.7e-009 1.29 46 7.9e-006 1.2e-002 5.1e-004 1.00e+000 3.573346130e+002 3.573541078e+002 4.3e-009 1.31 47 7.1e-006 1.2e-002 4.5e-004 1.00e+000 3.573360130e+002 3.573535584e+002 3.8e-009 1.33 48 6.4e-006 1.1e-002 4.1e-004 1.00e+000 3.573372731e+002 3.573530640e+002 3.5e-009 1.36 49 5.8e-006 1.1e-002 3.7e-004 1.00e+000 3.573384074e+002 3.573526192e+002 3.1e-009 1.37 50 5.2e-006 1.0e-002 3.3e-004 1.00e+000 3.573394283e+002 3.573522189e+002 2.8e-009 1.39 51 4.7e-006 1.0e-002 3.0e-004 1.00e+000 3.573403472e+002 3.573518587e+002 2.5e-009 1.40 52 4.2e-006 9.8e-003 2.7e-004 1.00e+000 3.573411742e+002 3.573515347e+002 2.3e-009 1.42 53 3.8e-006 9.6e-003 2.4e-004 1.00e+000 3.573419186e+002 3.573512430e+002 2.0e-009 1.44 54 3.4e-006 9.3e-003 2.2e-004 1.00e+000 3.573425885e+002 3.573509805e+002 1.8e-009 1.45 55 3.1e-006 9.1e-003 2.0e-004 1.00e+000 3.573431914e+002 3.573507443e+002 1.7e-009 1.47 56 2.8e-006 8.9e-003 1.8e-004 1.00e+000 3.573437340e+002 3.573505316e+002 1.5e-009 1.48 57 2.5e-006 8.8e-003 1.6e-004 1.00e+000 3.573442224e+002 3.573503402e+002 1.3e-009 1.51 58 2.2e-006 8.6e-003 1.4e-004 1.00e+000 3.573446619e+002 3.573501679e+002 1.2e-009 1.53 59 2.0e-006 8.5e-003 1.3e-004 1.00e+000 3.573450574e+002 3.573500129e+002 1.1e-009 1.54 60 1.8e-006 8.4e-003 1.2e-004 1.00e+000 3.573454134e+002 3.573498733e+002 9.7e-010 1.56 61 1.6e-006 8.2e-003 1.0e-004 1.00e+000 3.573457337e+002 3.573497477e+002 8.8e-010 1.58 62 1.5e-006 8.1e-003 9.4e-005 1.00e+000 3.573460220e+002 3.573496346e+002 7.9e-010 1.59 63 1.3e-006 8.1e-003 8.4e-005 1.00e+000 3.573462815e+002 3.573495328e+002 7.1e-010 1.61 64 1.2e-006 8.0e-003 7.6e-005 1.00e+000 3.573465150e+002 3.573494412e+002 6.4e-010 1.62 65 1.1e-006 7.9e-003 6.8e-005 1.00e+000 3.573467251e+002 3.573493587e+002 5.8e-010 1.64 66 9.6e-007 7.8e-003 6.1e-005 1.00e+000 3.573469142e+002 3.573492845e+002 5.2e-010 1.65 67 8.7e-007 7.8e-003 5.5e-005 1.00e+000 3.573470844e+002 3.573492177e+002 4.7e-010 1.69 68 7.8e-007 7.7e-003 5.0e-005 1.00e+000 3.573472376e+002 3.573491575e+002 4.2e-010 1.72 69 7.0e-007 7.7e-003 4.5e-005 1.00e+000 3.573473754e+002 3.573491033e+002 3.8e-010 1.75 70 6.3e-007 7.6e-003 4.0e-005 1.00e+000 3.573474995e+002 3.573490545e+002 3.4e-010 1.78 71 5.7e-007 7.6e-003 3.6e-005 1.00e+000 3.573476111e+002 3.573490106e+002 3.1e-010 1.79 72 5.1e-007 7.6e-003 3.3e-005 1.00e+000 3.573477115e+002 3.573489711e+002 2.8e-010 1.83 73 4.6e-007 7.5e-003 2.9e-005 1.00e+000 3.573478019e+002 3.573489355e+002 2.5e-010 1.86 74 4.1e-007 7.5e-003 2.6e-005 1.00e+000 3.573478832e+002 3.573489035e+002 2.2e-010 1.87 75 3.7e-007 7.5e-003 2.4e-005 1.00e+000 3.573479564e+002 3.573488746e+002 2.0e-010 1.90 76 3.4e-007 7.4e-003 2.1e-005 9.99e-001 3.573480223e+002 3.573488487e+002 1.8e-010 1.92 77 3.0e-007 7.4e-003 1.9e-005 1.00e+000 3.573480815e+002 3.573488253e+002 1.6e-010 1.93 78 2.7e-007 7.4e-003 1.7e-005 9.99e-001 3.573481348e+002 3.573488043e+002 1.5e-010 1.95 79 2.4e-007 7.4e-003 1.6e-005 1.00e+000 3.573481828e+002 3.573487854e+002 1.3e-010 1.97 80 2.2e-007 7.4e-003 1.4e-005 1.00e+000 3.573482261e+002 3.573487682e+002 1.2e-010 1.98 81 2.0e-007 6.6e-003 1.3e-005 1.00e+000 3.573482653e+002 3.573487527e+002 1.1e-010 2.00 82 1.8e-007 6.0e-003 1.1e-005 1.00e+000 3.573483002e+002 3.573487389e+002 9.6e-011 2.01 83 1.6e-007 5.4e-003 1.0e-005 1.00e+000 3.573483316e+002 3.573487264e+002 8.6e-011 2.04 84 1.4e-007 4.8e-003 9.2e-006 9.98e-001 3.573483599e+002 3.573487153e+002 7.8e-011 2.06 85 1.3e-007 4.4e-003 8.3e-006 9.99e-001 3.573483854e+002 3.573487052e+002 7.0e-011 2.08 86 1.2e-007 3.9e-003 7.5e-006 1.00e+000 3.573484083e+002 3.573486961e+002 6.3e-011 2.09 87 1.1e-007 3.5e-003 6.7e-006 1.00e+000 3.573484292e+002 3.573486878e+002 5.7e-011 2.11 88 9.5e-008 3.2e-003 6.1e-006 1.00e+000 3.573484478e+002 3.573486804e+002 5.1e-011 2.12 89 8.5e-008 2.9e-003 5.4e-006 9.98e-001 3.573484645e+002 3.573486738e+002 4.6e-011 2.14 90 7.7e-008 2.6e-003 4.9e-006 1.00e+000 3.573484797e+002 3.573486678e+002 4.2e-011 2.15 91 6.9e-008 2.3e-003 4.4e-006 1.00e+000 3.573484932e+002 3.573486624e+002 3.7e-011 2.17 92 6.2e-008 2.1e-003 4.0e-006 1.00e+000 3.573485054e+002 3.573486576e+002 3.4e-011 2.18 93 7.2e-009 2.2e-004 4.3e-007 9.99e-001 3.573486027e+002 3.573486190e+002 3.6e-012 2.20 94 6.5e-009 2.0e-004 3.8e-007 9.28e-001 3.573486039e+002 3.573486186e+002 3.3e-012 2.21 95 5.9e-009 1.8e-004 3.5e-007 1.21e+000 3.573486049e+002 3.573486181e+002 2.9e-012 2.25 96 5.3e-009 1.6e-004 3.1e-007 9.94e-001 3.573486059e+002 3.573486177e+002 2.6e-012 2.26 97 4.8e-009 1.5e-004 2.8e-007 9.78e-001 3.573486067e+002 3.573486174e+002 2.4e-012 2.28 98 2.9e-010 8.0e-006 1.5e-008 1.00e+000 3.573486140e+002 3.573486145e+002 1.3e-013 2.29 Interior-point optimizer terminated. Time: 2.29. Optimizer terminated. Time: 2.33 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.5734861396e+002 Viol. con: 4e-009 var: 0e+000 Dual. obj: 3.5734861455e+002 Viol. con: 0e+000 var: 6e-005 * End solution on dual form. * Transforming to primal solution. Solving took 2.34 seconds. result packing took 13% of solve time solution checking took 5.6% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Windows/64-X86 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1014 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.01 Lin. dep. - number : 0 Presolve terminated. Time: 0.05 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.06 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.67e+004 after factor : 1.73e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.290681039e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 6.1e+004 -9.71e-001 -1.268215792e+005 3.803698289e+000 4.7e-001 0.14 2 4.4e+002 5.7e+002 2.5e+004 -9.35e-001 -1.209150223e+005 1.085395626e+001 1.9e-001 0.16 3 2.9e+002 3.7e+002 1.6e+004 -8.42e-001 -1.160832565e+005 6.170096874e+001 1.3e-001 0.17 4 2.9e+002 3.7e+002 1.6e+004 -7.60e-001 -1.138839351e+005 1.952312349e+003 1.3e-001 0.20 5 8.6e+001 1.1e+002 4.8e+003 -7.56e-001 -7.867318473e+004 1.032812139e+004 3.8e-002 0.22 6 2.8e+001 3.7e+001 1.6e+003 -2.73e-001 -3.695942432e+004 1.216953342e+004 1.3e-002 0.23 7 1.4e+001 1.8e+001 7.7e+002 4.39e-001 -2.032946774e+004 6.163395773e+003 6.0e-003 0.25 8 7.5e+000 9.8e+000 4.3e+002 7.35e-001 -1.177598014e+004 3.686886489e+003 3.3e-003 0.28 9 2.9e+000 3.8e+000 1.6e+002 8.70e-001 -4.523320668e+003 1.603991647e+003 1.3e-003 0.30 10 1.4e+000 1.8e+000 7.8e+001 9.70e-001 -1.988525936e+003 9.573950568e+002 6.1e-004 0.31 11 9.5e-001 1.2e+000 5.4e+001 9.89e-001 -1.378341888e+003 6.922207403e+002 4.3e-004 0.33 12 8.3e-001 1.1e+000 4.7e+001 9.73e-001 -1.213234524e+003 6.052054907e+002 3.7e-004 0.34 13 3.4e-001 4.4e-001 1.9e+001 9.85e-001 -4.778949678e+002 2.688887630e+002 1.5e-004 0.37 14 1.7e-001 2.4e-001 9.9e+000 1.01e+000 -2.231453989e+002 1.590241696e+002 7.9e-005 0.39 15 5.8e-002 1.3e-001 3.4e+000 9.99e-001 -5.408005007e+001 7.790624611e+001 2.8e-005 0.41 16 2.6e-002 8.8e-002 1.6e+000 1.00e+000 -5.013955129e+000 5.511669305e+001 1.3e-005 0.42 17 1.4e-002 7.5e-002 8.6e-001 1.00e+000 1.335856339e+001 4.628977693e+001 7.0e-006 0.44 18 3.3e-003 1.2e-001 2.0e-001 1.00e+000 3.088416179e+001 3.862094009e+001 1.7e-006 0.47 19 2.0e-003 8.9e-002 1.3e-001 1.00e+000 3.292348922e+001 3.773142012e+001 1.0e-006 0.48 20 5.8e-004 1.0e-001 3.6e-002 1.00e+000 3.529664884e+001 3.667076487e+001 3.0e-007 0.50 21 2.6e-004 8.4e-002 1.6e-002 1.00e+000 3.582432208e+001 3.643126620e+001 1.3e-007 0.52 22 2.3e-004 7.6e-002 1.4e-002 1.00e+000 3.586897426e+001 3.641524576e+001 1.2e-007 0.53 23 1.4e-004 6.2e-002 8.4e-003 1.00e+000 3.602182237e+001 3.634497824e+001 7.0e-008 0.56 24 1.2e-004 5.6e-002 7.6e-003 1.00e+000 3.604448674e+001 3.633532407e+001 6.3e-008 0.58 25 1.1e-004 5.1e-002 6.8e-003 1.00e+000 3.606444928e+001 3.632618848e+001 5.7e-008 0.59 26 9.9e-005 4.7e-002 6.2e-003 1.00e+000 3.608239239e+001 3.631794692e+001 5.1e-008 0.61 27 8.9e-005 4.3e-002 5.5e-003 1.00e+000 3.609852558e+001 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39 2.5e-005 1.7e-002 1.6e-003 1.00e+000 3.620250871e+001 3.626236457e+001 1.3e-008 0.95 40 2.3e-005 1.6e-002 1.4e-003 1.00e+000 3.620659448e+001 3.626046423e+001 1.2e-008 0.98 41 2.0e-005 1.5e-002 1.3e-003 1.00e+000 3.621027126e+001 3.625875360e+001 1.1e-008 1.01 42 1.8e-005 1.5e-002 1.1e-003 1.00e+000 3.621358000e+001 3.625721378e+001 9.5e-009 1.04 43 1.7e-005 1.4e-002 1.0e-003 1.00e+000 3.621655759e+001 3.625582773e+001 8.6e-009 1.06 44 1.5e-005 1.3e-002 9.2e-004 1.00e+000 3.621923717e+001 3.625458009e+001 7.7e-009 1.09 45 1.3e-005 1.3e-002 8.3e-004 1.00e+000 3.622164859e+001 3.625345705e+001 6.9e-009 1.12 46 1.2e-005 1.2e-002 7.5e-004 1.00e+000 3.622381870e+001 3.625244618e+001 6.2e-009 1.15 47 1.1e-005 1.2e-002 6.7e-004 1.00e+000 3.622577163e+001 3.625153626e+001 5.6e-009 1.19 48 9.8e-006 1.1e-002 6.1e-004 1.00e+000 3.622752913e+001 3.625071722e+001 5.1e-009 1.22 49 8.8e-006 1.1e-002 5.5e-004 1.00e+000 3.622911076e+001 3.624997998e+001 4.5e-009 1.25 50 7.9e-006 1.0e-002 4.9e-004 1.00e+000 3.623053411e+001 3.624931636e+001 4.1e-009 1.28 51 7.1e-006 1.0e-002 4.4e-004 1.00e+000 3.623181501e+001 3.624871903e+001 3.7e-009 1.33 52 6.4e-006 9.8e-003 4.0e-004 1.00e+000 3.623296773e+001 3.624818133e+001 3.3e-009 1.36 53 5.8e-006 9.5e-003 3.6e-004 1.00e+000 3.623400510e+001 3.624769732e+001 3.0e-009 1.40 54 5.2e-006 9.3e-003 3.2e-004 1.00e+000 3.623493865e+001 3.624726164e+001 2.7e-009 1.44 55 4.7e-006 9.1e-003 2.9e-004 1.00e+000 3.623577877e+001 3.624686947e+001 2.4e-009 1.48 56 4.2e-006 8.9e-003 2.6e-004 1.00e+000 3.623653481e+001 3.624651645e+001 2.2e-009 1.51 57 3.8e-006 8.7e-003 2.3e-004 1.00e+000 3.623721519e+001 3.624619868e+001 2.0e-009 1.54 58 3.4e-006 8.6e-003 2.1e-004 1.00e+000 3.623782749e+001 3.624591262e+001 1.8e-009 1.58 59 3.1e-006 8.4e-003 1.9e-004 1.00e+000 3.623837850e+001 3.624565513e+001 1.6e-009 1.61 60 2.8e-006 8.3e-003 1.7e-004 1.00e+000 3.623887437e+001 3.624542335e+001 1.4e-009 1.64 61 2.5e-006 8.2e-003 1.5e-004 1.00e+000 3.623932061e+001 3.624521470e+001 1.3e-009 1.67 62 2.2e-006 8.1e-003 1.4e-004 1.00e+000 3.623972220e+001 3.624502688e+001 1.2e-009 1.70 63 2.0e-006 8.0e-003 1.2e-004 1.00e+000 3.624008359e+001 3.624485781e+001 1.0e-009 1.73 64 1.8e-006 7.9e-003 1.1e-004 1.00e+000 3.624040882e+001 3.624470562e+001 9.4e-010 1.76 65 1.6e-006 7.8e-003 1.0e-004 1.00e+000 3.624070151e+001 3.624456862e+001 8.4e-010 1.79 66 1.5e-006 7.8e-003 9.1e-005 1.00e+000 3.624096490e+001 3.624444531e+001 7.6e-010 1.81 67 1.3e-006 7.7e-003 8.2e-005 1.00e+000 3.624120193e+001 3.624433430e+001 6.8e-010 1.84 68 1.2e-006 7.6e-003 7.4e-005 1.00e+000 3.624141524e+001 3.624423439e+001 6.1e-010 1.87 69 1.1e-006 7.6e-003 6.6e-005 1.00e+000 3.624160721e+001 3.624414445e+001 5.5e-010 1.90 70 9.6e-007 7.5e-003 6.0e-005 1.00e+000 3.624177997e+001 3.624406350e+001 5.0e-010 1.93 71 8.6e-007 7.5e-003 5.4e-005 1.00e+000 3.624193543e+001 3.624399063e+001 4.5e-010 1.97 72 7.8e-007 7.5e-003 4.8e-005 1.00e+000 3.624207535e+001 3.624392502e+001 4.0e-010 2.01 73 7.0e-007 7.4e-003 4.4e-005 1.00e+000 3.624220126e+001 3.624386598e+001 3.6e-010 2.04 74 6.3e-007 7.4e-003 3.9e-005 1.00e+000 3.624231458e+001 3.624381282e+001 3.3e-010 2.08 75 5.7e-007 7.4e-003 3.5e-005 1.00e+000 3.624241655e+001 3.624376497e+001 2.9e-010 2.11 76 5.1e-007 7.3e-003 3.2e-005 1.00e+000 3.624250832e+001 3.624372191e+001 2.6e-010 2.15 77 4.6e-007 7.3e-003 2.9e-005 1.00e+000 3.624259092e+001 3.624368314e+001 2.4e-010 2.20 78 4.1e-007 7.3e-003 2.6e-005 1.00e+000 3.624266524e+001 3.624364824e+001 2.1e-010 2.25 79 3.7e-007 7.3e-003 2.3e-005 1.00e+000 3.624273213e+001 3.624361683e+001 1.9e-010 2.29 80 3.3e-007 7.2e-003 2.1e-005 1.00e+000 3.624279233e+001 3.624358856e+001 1.7e-010 2.32 81 3.0e-007 7.2e-003 1.9e-005 1.00e+000 3.624284650e+001 3.624356312e+001 1.6e-010 2.37 82 2.7e-007 7.2e-003 1.7e-005 1.00e+000 3.624289526e+001 3.624354021e+001 1.4e-010 2.42 83 2.4e-007 7.2e-003 1.5e-005 1.00e+000 3.624293914e+001 3.624351958e+001 1.3e-010 2.46 84 2.2e-007 7.2e-003 1.4e-005 1.00e+000 3.624297862e+001 3.624350103e+001 1.1e-010 2.50 85 2.0e-007 7.2e-003 1.2e-005 1.00e+000 3.624301416e+001 3.624348432e+001 1.0e-010 2.53 86 1.8e-007 7.1e-003 1.1e-005 1.00e+000 3.624304614e+001 3.624346929e+001 9.2e-011 2.56 87 1.6e-007 7.1e-003 1.0e-005 1.00e+000 3.624307492e+001 3.624345575e+001 8.3e-011 2.61 88 1.4e-007 7.1e-003 9.0e-006 9.99e-001 3.624310082e+001 3.624344358e+001 7.5e-011 2.65 89 1.3e-007 7.1e-003 8.1e-006 1.00e+000 3.624312413e+001 3.624343261e+001 6.7e-011 2.68 90 1.2e-007 7.1e-003 7.3e-006 1.00e+000 3.624314511e+001 3.624342275e+001 6.0e-011 2.73 91 1.1e-007 7.1e-003 6.5e-006 1.00e+000 3.624316400e+001 3.624341386e+001 5.4e-011 2.76 92 9.5e-008 7.1e-003 5.9e-006 1.00e+000 3.624318099e+001 3.624340585e+001 4.9e-011 2.81 93 8.5e-008 7.1e-003 5.3e-006 9.98e-001 3.624319628e+001 3.624339868e+001 4.4e-011 2.84 94 7.7e-008 7.1e-003 4.8e-006 1.00e+000 3.624321004e+001 3.624339220e+001 4.0e-011 2.89 95 6.9e-008 7.0e-003 4.3e-006 9.98e-001 3.624322242e+001 3.624338638e+001 3.6e-011 2.92 96 6.2e-008 7.0e-003 3.9e-006 1.00e+000 3.624323357e+001 3.624338113e+001 3.2e-011 2.96 97 5.6e-008 7.0e-003 3.5e-006 1.00e+000 3.624324360e+001 3.624337640e+001 2.9e-011 3.00 98 5.0e-008 7.0e-003 3.1e-006 1.00e+000 3.624325263e+001 3.624337215e+001 2.6e-011 3.04 99 4.5e-008 6.3e-003 2.8e-006 1.00e+000 3.624326085e+001 3.624336826e+001 2.3e-011 3.07 100 4.1e-008 5.7e-003 2.5e-006 9.99e-001 3.624326815e+001 3.624336483e+001 2.1e-011 3.10 101 3.7e-008 5.1e-003 2.3e-006 1.01e+000 3.624327491e+001 3.624336162e+001 1.9e-011 3.12 102 3.3e-008 4.6e-003 2.0e-006 1.00e+000 3.624328081e+001 3.624335884e+001 1.7e-011 3.15 103 3.0e-008 4.2e-003 1.8e-006 9.98e-001 3.624328612e+001 3.624335635e+001 1.5e-011 3.17 104 2.7e-008 3.7e-003 1.7e-006 1.00e+000 3.624329096e+001 3.624335406e+001 1.4e-011 3.18 105 2.4e-008 3.4e-003 1.5e-006 9.95e-001 3.624329524e+001 3.624335205e+001 1.3e-011 3.20 106 2.2e-008 3.0e-003 1.3e-006 1.00e+000 3.624329916e+001 3.624335020e+001 1.1e-011 3.23 107 1.9e-008 2.7e-003 1.2e-006 9.96e-001 3.624330263e+001 3.624334857e+001 1.0e-011 3.25 108 1.8e-008 2.5e-003 1.1e-006 1.00e+000 3.624330580e+001 3.624334707e+001 9.2e-012 3.26 109 1.6e-008 2.2e-003 9.8e-007 1.00e+000 3.624330861e+001 3.624334575e+001 8.2e-012 3.28 110 1.4e-008 2.0e-003 8.8e-007 9.96e-001 3.624331113e+001 3.624334457e+001 7.4e-012 3.29 111 1.3e-008 1.8e-003 7.9e-007 9.97e-001 3.624331340e+001 3.624334350e+001 6.7e-012 3.31 112 1.2e-008 1.6e-003 7.1e-007 1.00e+000 3.624331545e+001 3.624334254e+001 6.0e-012 3.34 113 1.0e-008 1.4e-003 6.4e-007 1.00e+000 3.624331729e+001 3.624334167e+001 5.4e-012 3.35 114 9.3e-009 1.3e-003 5.8e-007 9.98e-001 3.624331895e+001 3.624334089e+001 4.9e-012 3.37 115 8.4e-009 1.2e-003 5.2e-007 1.00e+000 3.624332044e+001 3.624334019e+001 4.4e-012 3.38 116 7.5e-009 1.1e-003 4.7e-007 9.99e-001 3.624332178e+001 3.624333955e+001 3.9e-012 3.42 117 6.8e-009 9.5e-004 4.2e-007 1.00e+000 3.624332299e+001 3.624333898e+001 3.5e-012 3.43 118 6.1e-009 8.5e-004 3.8e-007 1.00e+000 3.624332407e+001 3.624333847e+001 3.2e-012 3.45 119 5.5e-009 7.7e-004 3.4e-007 9.99e-001 3.624332505e+001 3.624333801e+001 2.9e-012 3.46 120 5.0e-009 6.9e-004 3.1e-007 1.00e+000 3.624332593e+001 3.624333760e+001 2.6e-012 3.48 121 4.5e-009 6.2e-004 2.8e-007 1.00e+000 3.624332673e+001 3.624333722e+001 2.3e-012 3.51 122 4.0e-009 5.6e-004 2.5e-007 9.99e-001 3.624332744e+001 3.624333688e+001 2.1e-012 3.53 123 3.6e-009 5.0e-004 2.2e-007 1.00e+000 3.624332809e+001 3.624333658e+001 1.9e-012 3.54 124 3.2e-009 4.5e-004 2.0e-007 1.00e+000 3.624332867e+001 3.624333630e+001 1.7e-012 3.56 125 2.9e-009 4.1e-004 1.8e-007 9.97e-001 3.624332919e+001 3.624333606e+001 1.5e-012 3.57 126 2.6e-009 3.7e-004 1.6e-007 9.99e-001 3.624332965e+001 3.624333584e+001 1.4e-012 3.60 127 2.4e-009 3.3e-004 1.5e-007 1.00e+000 3.624333007e+001 3.624333564e+001 1.2e-012 3.62 128 2.1e-009 3.0e-004 1.3e-007 9.98e-001 3.624333045e+001 3.624333546e+001 1.1e-012 3.63 129 1.9e-009 2.7e-004 1.2e-007 1.00e+000 3.624333079e+001 3.624333530e+001 1.0e-012 3.65 130 1.7e-009 2.4e-004 1.1e-007 9.94e-001 3.624333110e+001 3.624333516e+001 9.0e-013 3.67 Interior-point optimizer terminated. Time: 3.68. Optimizer terminated. Time: 3.70 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 3.6243331100e+001 Viol. con: 3e-008 var: 0e+000 Dual. obj: 3.6243335156e+001 Viol. con: 0e+000 var: 2e-003 * End solution on dual form. * Transforming to primal solution. Solving took 3.72 seconds. result packing took 9.9% of solve time solution checking took 2% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Windows/64-X86 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1014 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.05 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.06 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.67e+004 after factor : 1.73e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.290330703e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.267780811e+005 3.774544865e+000 4.7e-001 0.14 2 4.2e+002 5.5e+002 2.4e+004 -9.35e-001 -1.205610482e+005 1.084812298e+001 1.9e-001 0.16 3 2.8e+002 3.7e+002 1.6e+004 -8.37e-001 -1.159167736e+005 6.710097048e+001 1.3e-001 0.17 4 2.8e+002 3.7e+002 1.6e+004 -7.57e-001 -1.133273473e+005 2.271174864e+003 1.2e-001 0.20 5 7.5e+001 9.8e+001 4.2e+003 -7.51e-001 -7.361547660e+004 1.118285118e+004 3.3e-002 0.22 6 3.0e+001 4.0e+001 1.7e+003 -1.90e-001 -3.975467163e+004 1.104183285e+004 1.3e-002 0.23 7 1.4e+001 1.8e+001 7.8e+002 3.94e-001 -2.072233058e+004 5.965812303e+003 6.1e-003 0.25 8 9.0e+000 1.2e+001 5.1e+002 7.30e-001 -1.406341386e+004 4.089875286e+003 4.0e-003 0.27 9 3.6e+000 4.7e+000 2.1e+002 8.35e-001 -5.848801228e+003 1.818685492e+003 1.6e-003 0.28 10 2.0e+000 2.6e+000 1.1e+002 9.52e-001 -2.940275428e+003 1.322853009e+003 8.9e-004 0.31 11 9.0e-001 1.2e+000 5.1e+001 9.84e-001 -1.328456856e+003 6.211636243e+002 4.1e-004 0.33 12 8.6e-001 1.2e+000 4.9e+001 9.64e-001 -1.289368260e+003 5.827096525e+002 3.9e-004 0.34 13 3.8e-001 5.3e-001 2.2e+001 9.81e-001 -5.618031116e+002 2.734704162e+002 1.7e-004 0.38 14 1.5e-001 2.3e-001 8.6e+000 1.00e+000 -2.182138957e+002 1.114451976e+002 6.9e-005 0.39 15 8.5e-002 1.5e-001 5.0e+000 1.00e+000 -1.178903141e+002 7.362856015e+001 4.0e-005 0.41 16 2.6e-002 1.2e-001 1.6e+000 1.00e+000 -2.818159037e+001 3.133073639e+001 1.3e-005 0.44 17 1.1e-002 9.3e-002 6.9e-001 1.00e+000 -5.309147649e+000 2.122331187e+001 5.7e-006 0.45 18 1.0e-002 8.4e-002 6.3e-001 1.01e+000 -3.443357851e+000 2.059680462e+001 5.2e-006 0.47 19 6.6e-003 6.5e-002 4.0e-001 1.01e+000 2.877422758e+000 1.822759827e+001 3.3e-006 0.48 20 4.5e-003 4.7e-002 2.8e-001 1.01e+000 6.695367880e+000 1.712990839e+001 2.3e-006 0.50 21 1.8e-003 5.9e-002 1.1e-001 1.01e+000 1.119640064e+001 1.544776151e+001 9.4e-007 0.53 22 1.0e-003 4.8e-002 6.2e-002 1.02e+000 1.264781245e+001 1.495323164e+001 5.1e-007 0.55 23 4.6e-004 5.4e-002 2.9e-002 1.02e+000 1.351630183e+001 1.458915085e+001 2.4e-007 0.56 24 2.6e-004 5.1e-002 1.6e-002 1.01e+000 1.385918914e+001 1.445496319e+001 1.3e-007 0.59 25 1.3e-004 5.2e-002 8.5e-003 1.01e+000 1.406173786e+001 1.437377172e+001 7.1e-008 0.61 26 8.9e-005 4.6e-002 5.6e-003 1.01e+000 1.413619115e+001 1.434330369e+001 4.7e-008 0.62 27 8.0e-005 4.2e-002 5.1e-003 1.00e+000 1.415442751e+001 1.434090157e+001 4.3e-008 0.66 28 7.2e-005 3.9e-002 4.6e-003 1.00e+000 1.416707194e+001 1.433486570e+001 3.8e-008 0.67 29 6.5e-005 3.6e-002 4.1e-003 1.00e+000 1.417868457e+001 1.432967871e+001 3.4e-008 0.69 30 5.9e-005 3.3e-002 3.7e-003 1.00e+000 1.418908203e+001 1.432495998e+001 3.1e-008 0.72 31 5.3e-005 3.0e-002 3.3e-003 1.00e+000 1.419841859e+001 1.432069511e+001 2.8e-008 0.73 32 4.8e-005 2.8e-002 3.0e-003 1.00e+000 1.420680032e+001 1.431683734e+001 2.5e-008 0.75 33 4.3e-005 2.6e-002 2.7e-003 1.00e+000 1.421432588e+001 1.431334932e+001 2.3e-008 0.77 34 3.8e-005 2.4e-002 2.4e-003 1.00e+000 1.422108358e+001 1.431019724e+001 2.0e-008 0.80 35 3.5e-005 2.2e-002 2.2e-003 1.00e+000 1.422715304e+001 1.430734879e+001 1.8e-008 0.81 36 3.1e-005 2.1e-002 2.0e-003 1.00e+000 1.423260585e+001 1.430477776e+001 1.6e-008 0.83 37 2.8e-005 2.0e-002 1.8e-003 1.00e+000 1.423750549e+001 1.430245663e+001 1.5e-008 0.84 38 2.5e-005 1.8e-002 1.6e-003 1.00e+000 1.424190905e+001 1.430036216e+001 1.3e-008 0.87 39 2.3e-005 1.7e-002 1.4e-003 1.00e+000 1.424586728e+001 1.429847270e+001 1.2e-008 0.89 40 2.0e-005 1.6e-002 1.3e-003 1.00e+000 1.424942563e+001 1.429676883e+001 1.1e-008 0.91 41 1.8e-005 1.5e-002 1.2e-003 1.00e+000 1.425262483e+001 1.429523189e+001 9.7e-009 0.92 42 1.7e-005 1.5e-002 1.0e-003 1.00e+000 1.425550152e+001 1.429384596e+001 8.8e-009 0.95 43 1.5e-005 1.4e-002 9.4e-004 1.00e+000 1.425808823e+001 1.429259743e+001 7.9e-009 0.97 44 1.3e-005 1.3e-002 8.5e-004 1.00e+000 1.426041432e+001 1.429147083e+001 7.1e-009 0.98 45 1.2e-005 1.3e-002 7.6e-004 1.00e+000 1.426250616e+001 1.429045655e+001 6.4e-009 1.01 46 1.1e-005 1.2e-002 6.9e-004 1.00e+000 1.426438709e+001 1.428954279e+001 5.7e-009 1.03 47 9.8e-006 1.2e-002 6.2e-004 1.00e+000 1.426607863e+001 1.428871788e+001 5.2e-009 1.06 48 8.8e-006 1.1e-002 5.5e-004 1.00e+000 1.426759974e+001 1.428797506e+001 4.7e-009 1.09 49 7.9e-006 1.1e-002 5.0e-004 1.00e+000 1.426896751e+001 1.428730491e+001 4.2e-009 1.11 50 7.1e-006 1.1e-002 4.5e-004 1.00e+000 1.427019734e+001 1.428670092e+001 3.8e-009 1.14 51 6.4e-006 1.0e-002 4.0e-004 1.00e+000 1.427130316e+001 1.428615606e+001 3.4e-009 1.17 52 5.8e-006 1.0e-002 3.6e-004 1.00e+000 1.427229746e+001 1.428566485e+001 3.1e-009 1.20 53 5.2e-006 9.7e-003 3.3e-004 1.00e+000 1.427319149e+001 1.428522226e+001 2.7e-009 1.22 54 4.7e-006 9.5e-003 2.9e-004 1.00e+000 1.427399549e+001 1.428482316e+001 2.5e-009 1.25 55 4.2e-006 9.3e-003 2.7e-004 1.00e+000 1.427471885e+001 1.428446237e+001 2.2e-009 1.28 56 3.8e-006 9.1e-003 2.4e-004 9.99e-001 1.427536920e+001 1.428413896e+001 2.0e-009 1.29 57 3.4e-006 9.0e-003 2.2e-004 1.00e+000 1.427595431e+001 1.428384699e+001 1.8e-009 1.33 58 3.1e-006 8.8e-003 1.9e-004 1.00e+000 1.427648075e+001 1.428358395e+001 1.6e-009 1.36 59 2.8e-006 8.7e-003 1.7e-004 9.99e-001 1.427695427e+001 1.428334753e+001 1.5e-009 1.40 60 2.5e-006 8.5e-003 1.6e-004 1.00e+000 1.427738037e+001 1.428313436e+001 1.3e-009 1.47 61 2.2e-006 8.4e-003 1.4e-004 1.00e+000 1.427776378e+001 1.428294239e+001 1.2e-009 1.50 62 2.0e-006 8.3e-003 1.3e-004 9.96e-001 1.427810856e+001 1.428277039e+001 1.1e-009 1.54 63 1.8e-006 8.2e-003 1.1e-004 9.97e-001 1.427841886e+001 1.428261516e+001 9.6e-010 1.59 64 1.6e-006 8.1e-003 1.0e-004 1.00e+000 1.427869831e+001 1.428247450e+001 8.6e-010 1.62 65 1.5e-006 8.1e-003 9.3e-005 1.00e+000 1.427895013e+001 1.428234764e+001 7.8e-010 1.67 66 1.3e-006 8.0e-003 8.3e-005 9.96e-001 1.427917617e+001 1.428223455e+001 7.0e-010 1.72 67 1.2e-006 7.9e-003 7.5e-005 1.00e+000 1.427938053e+001 1.428213142e+001 6.3e-010 1.75 68 1.1e-006 7.9e-003 6.7e-005 9.97e-001 1.427956352e+001 1.428203970e+001 5.7e-010 1.78 69 9.6e-007 7.8e-003 6.1e-005 1.00e+000 1.427972822e+001 1.428195685e+001 5.1e-010 1.83 70 8.7e-007 7.8e-003 5.5e-005 1.00e+000 1.427987648e+001 1.428188212e+001 4.6e-010 1.86 71 7.8e-007 7.7e-003 4.9e-005 9.95e-001 1.428000978e+001 1.428181535e+001 4.1e-010 1.90 72 7.0e-007 7.7e-003 4.4e-005 1.00e+000 1.428012981e+001 1.428175486e+001 3.7e-010 1.94 73 6.3e-007 7.7e-003 4.0e-005 1.00e+000 1.428023833e+001 1.428169997e+001 3.3e-010 1.98 74 5.7e-007 6.9e-003 3.6e-005 1.01e+000 1.428033930e+001 1.428164854e+001 3.0e-010 2.01 75 5.1e-007 6.2e-003 3.2e-005 9.92e-001 1.428042627e+001 1.428160508e+001 2.7e-010 2.04 76 4.6e-007 5.6e-003 2.9e-005 1.00e+000 1.428050556e+001 1.428156488e+001 2.5e-010 2.09 77 4.1e-007 5.0e-003 2.6e-005 1.00e+000 1.428057600e+001 1.428152929e+001 2.2e-010 2.12 78 3.7e-007 4.5e-003 2.4e-005 1.02e+000 1.428064360e+001 1.428149466e+001 2.0e-010 2.15 79 3.4e-007 4.1e-003 2.1e-005 9.83e-001 1.428070007e+001 1.428146669e+001 1.8e-010 2.18 80 3.0e-007 3.7e-003 1.9e-005 9.82e-001 1.428075088e+001 1.428144147e+001 1.6e-010 2.21 81 2.7e-007 3.3e-003 1.7e-005 1.03e+000 1.428080182e+001 1.428141507e+001 1.5e-010 2.26 82 2.5e-007 3.0e-003 1.5e-005 9.83e-001 1.428084250e+001 1.428139489e+001 1.3e-010 2.29 83 2.2e-007 2.7e-003 1.4e-005 9.76e-001 1.428087906e+001 1.428137681e+001 1.2e-010 2.33 84 2.0e-007 2.4e-003 1.3e-005 9.83e-001 1.428091201e+001 1.428136037e+001 1.1e-010 2.37 85 1.8e-007 2.2e-003 1.1e-005 9.98e-001 1.428094173e+001 1.428134528e+001 9.7e-011 2.40 86 1.6e-007 1.9e-003 1.0e-005 1.02e+000 1.428097060e+001 1.428133035e+001 8.8e-011 2.43 87 1.4e-007 1.8e-003 9.1e-006 9.89e-001 1.428099443e+001 1.428131839e+001 7.9e-011 2.48 88 1.3e-007 1.6e-003 8.2e-006 1.00e+000 1.428101598e+001 1.428130742e+001 7.1e-011 2.51 89 1.2e-007 1.4e-003 7.4e-006 9.83e-001 1.428103526e+001 1.428129778e+001 6.4e-011 2.56 90 1.1e-007 1.3e-003 6.6e-006 1.07e+000 1.428105813e+001 1.428128539e+001 6.0e-011 2.59 91 9.5e-008 1.2e-003 6.0e-006 9.78e-001 1.428107319e+001 1.428127797e+001 5.4e-011 2.62 92 8.5e-008 1.0e-003 5.4e-006 1.08e+000 1.428109183e+001 1.428126783e+001 5.0e-011 2.65 93 7.7e-008 9.3e-004 4.8e-006 1.07e+000 1.428110711e+001 1.428125975e+001 4.7e-011 2.68 94 7.1e-008 8.4e-004 4.4e-006 1.16e+000 1.428112507e+001 1.428124954e+001 4.6e-011 2.71 95 6.4e-008 7.6e-004 3.9e-006 9.33e-001 1.428113340e+001 1.428124580e+001 4.1e-011 2.75 96 5.7e-008 6.8e-004 3.5e-006 1.05e+000 1.428114256e+001 1.428124118e+001 3.8e-011 2.78 97 5.2e-008 6.1e-004 3.2e-006 9.76e-001 1.428114920e+001 1.428123806e+001 3.4e-011 2.81 98 4.6e-008 5.5e-004 2.9e-006 1.03e+000 1.428115587e+001 1.428123477e+001 3.1e-011 2.84 99 4.2e-008 5.0e-004 2.6e-006 1.07e+000 1.428116290e+001 1.428123117e+001 2.9e-011 2.87 100 3.8e-008 4.5e-004 2.3e-006 9.50e-001 1.428116749e+001 1.428122909e+001 2.6e-011 2.92 101 3.4e-008 4.0e-004 2.1e-006 9.52e-001 1.428117162e+001 1.428122719e+001 2.3e-011 2.96 102 3.0e-008 3.6e-004 1.9e-006 8.37e-001 1.428117528e+001 1.428122570e+001 2.1e-011 3.00 103 2.7e-008 3.3e-004 1.7e-006 9.93e-001 1.428117866e+001 1.428122406e+001 1.9e-011 3.03 104 2.4e-008 2.9e-004 1.5e-006 1.01e+000 1.428118187e+001 1.428122246e+001 1.7e-011 3.06 105 2.2e-008 2.6e-004 1.4e-006 1.00e+000 1.428118460e+001 1.428122112e+001 1.5e-011 3.09 106 2.0e-008 2.4e-004 1.2e-006 9.81e-001 1.428118705e+001 1.428121995e+001 1.4e-011 3.14 107 1.8e-008 2.1e-004 1.1e-006 1.04e+000 1.428118959e+001 1.428121865e+001 1.3e-011 3.17 108 1.6e-008 1.9e-004 1.0e-006 9.93e-001 1.428119154e+001 1.428121770e+001 1.1e-011 3.20 109 1.4e-008 1.7e-004 9.0e-007 1.01e+000 1.428119334e+001 1.428121682e+001 1.0e-011 3.23 110 1.3e-008 1.6e-004 8.1e-007 9.83e-001 1.428119491e+001 1.428121607e+001 9.3e-012 3.28 111 1.2e-008 1.4e-004 7.3e-007 9.98e-001 1.428119633e+001 1.428121538e+001 8.4e-012 3.31 112 1.1e-008 1.3e-004 6.5e-007 1.01e+000 1.428119768e+001 1.428121471e+001 7.6e-012 3.34 113 9.5e-009 1.1e-004 5.9e-007 1.06e+000 1.428119912e+001 1.428121396e+001 7.0e-012 3.37 114 8.6e-009 1.0e-004 5.3e-007 1.10e+000 1.428120055e+001 1.428121318e+001 6.6e-012 3.40 115 7.8e-009 9.2e-005 4.8e-007 1.00e+000 1.428120141e+001 1.428121278e+001 6.0e-012 3.45 116 7.0e-009 8.3e-005 4.3e-007 9.84e-001 1.428120218e+001 1.428121242e+001 5.4e-012 3.48 117 6.3e-009 7.4e-005 3.9e-007 9.26e-001 1.428120287e+001 1.428121212e+001 4.8e-012 3.51 118 5.6e-009 6.7e-005 3.5e-007 9.36e-001 1.428120349e+001 1.428121184e+001 4.4e-012 3.54 119 5.1e-009 6.0e-005 3.1e-007 1.03e+000 1.428120412e+001 1.428121153e+001 4.0e-012 3.57 120 4.0e-009 3.7e-006 1.9e-008 8.54e-001 1.428120902e+001 1.428120952e+001 4.8e-013 3.62 Interior-point optimizer terminated. Time: 3.62. Optimizer terminated. Time: 3.63 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.4281209023e+001 Viol. con: 9e-008 var: 0e+000 Dual. obj: 1.4281209516e+001 Viol. con: 0e+000 var: 2e-005 * End solution on dual form. * Transforming to primal solution. Solving took 3.66 seconds. result packing took 8.6% of solve time solution checking took 3.6% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Windows/64-X86 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1010 Eliminator terminated. Eliminator started. Total number of eliminations : 1022 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1022 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.05 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 831 Optimizer - Cones : 0 Optimizer - Scalar variables : 3583 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.06 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.68e+004 after factor : 1.73e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.290574277e+005 2.000000000e+000 1.0e+000 0.11 1 1.1e+003 1.4e+003 6.0e+004 -9.71e-001 -1.267593448e+005 3.779138571e+000 4.6e-001 0.14 2 4.0e+002 5.1e+002 2.2e+004 -9.34e-001 -1.199975494e+005 1.136909795e+001 1.7e-001 0.16 3 2.8e+002 3.7e+002 1.6e+004 -8.29e-001 -1.158572172e+005 8.355280206e+001 1.2e-001 0.19 4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.125565121e+005 2.829427599e+003 1.2e-001 0.20 5 6.3e+001 8.2e+001 3.6e+003 -7.47e-001 -6.652020764e+004 1.269515030e+004 2.8e-002 0.22 6 3.9e+001 5.1e+001 2.2e+003 -7.23e-002 -4.867285388e+004 1.113591078e+004 1.7e-002 0.23 7 2.8e+001 3.7e+001 1.6e+003 2.50e-001 -3.845378484e+004 8.760244184e+003 1.3e-002 0.27 8 1.6e+001 2.1e+001 9.0e+002 4.35e-001 -2.431729960e+004 5.454866729e+003 7.1e-003 0.30 9 6.4e+000 8.4e+000 3.6e+002 6.74e-001 -1.033759657e+004 2.808730926e+003 2.9e-003 0.34 10 3.6e+000 4.7e+000 2.0e+002 8.88e-001 -5.652148454e+003 1.901726748e+003 1.6e-003 0.36 11 1.3e+000 1.7e+000 7.4e+001 9.54e-001 -2.009808258e+003 7.858141941e+002 5.9e-004 0.38 12 1.0e+000 1.3e+000 5.7e+001 9.87e-001 -1.519705847e+003 6.348797112e+002 4.5e-004 0.41 13 8.5e-001 1.5e+000 4.8e+001 9.70e-001 -1.298289371e+003 5.488322141e+002 3.8e-004 0.42 14 2.9e-001 5.1e-001 1.6e+001 9.89e-001 -4.338195618e+002 1.968234619e+002 1.3e-004 0.44 15 1.6e-001 3.0e-001 9.4e+000 1.00e+000 -2.406885176e+002 1.171939970e+002 7.5e-005 0.45 16 7.3e-002 1.6e-001 4.3e+000 1.00e+000 -1.045666489e+002 5.782855621e+001 3.4e-005 0.48 17 3.5e-002 1.0e-001 2.1e+000 1.01e+000 -4.669092481e+001 3.252115448e+001 1.7e-005 0.50 18 1.8e-002 7.9e-002 1.1e+000 1.01e+000 -2.055590143e+001 2.049383318e+001 8.8e-006 0.52 19 1.8e-002 7.6e-002 1.0e+000 1.02e+000 -1.909312644e+001 2.048700487e+001 8.5e-006 0.53 20 9.5e-003 5.8e-002 5.6e-001 1.02e+000 -4.512979643e+000 1.659855766e+001 4.6e-006 0.55 21 4.1e-003 5.7e-002 2.4e-001 1.02e+000 4.603740001e+000 1.368130039e+001 2.0e-006 0.56 22 2.2e-003 5.2e-002 1.3e-001 1.01e+000 7.750177327e+000 1.261803882e+001 1.1e-006 0.59 23 6.0e-004 8.2e-002 3.9e-002 9.87e-001 1.034186521e+001 1.181253534e+001 3.4e-007 0.61 24 1.8e-004 8.8e-002 1.3e-002 9.79e-001 1.109021531e+001 1.156965983e+001 1.1e-007 0.62 25 6.0e-005 8.7e-002 4.3e-003 9.88e-001 1.133223991e+001 1.149501150e+001 3.9e-008 0.64 26 2.2e-005 8.4e-002 1.6e-003 9.96e-001 1.141321581e+001 1.147321428e+001 1.5e-008 0.67 27 8.2e-006 8.1e-002 6.0e-004 9.99e-001 1.144290511e+001 1.146574209e+001 5.6e-009 0.69 28 7.4e-006 7.4e-002 5.4e-004 1.00e+000 1.144483377e+001 1.146538993e+001 5.0e-009 0.70 29 6.7e-006 6.7e-002 4.9e-004 1.00e+000 1.144642817e+001 1.146492920e+001 4.5e-009 0.72 30 6.0e-006 6.1e-002 4.4e-004 1.00e+000 1.144786288e+001 1.146451418e+001 4.1e-009 0.73 31 5.4e-006 5.6e-002 3.9e-004 1.00e+000 1.144915148e+001 1.146413788e+001 3.7e-009 0.77 32 4.9e-006 5.1e-002 3.5e-004 1.00e+000 1.145031003e+001 1.146379806e+001 3.3e-009 0.78 33 4.4e-006 4.6e-002 3.2e-004 1.00e+000 1.145135158e+001 1.146349095e+001 3.0e-009 0.81 34 3.9e-006 4.2e-002 2.9e-004 1.00e+000 1.145228808e+001 1.146321357e+001 2.7e-009 0.84 35 3.5e-006 3.9e-002 2.6e-004 1.00e+000 1.145313019e+001 1.146296321e+001 2.4e-009 0.87 36 3.2e-006 3.6e-002 2.3e-004 1.00e+000 1.145388748e+001 1.146273729e+001 2.2e-009 0.91 37 2.9e-006 3.3e-002 2.1e-004 1.00e+000 1.145456859e+001 1.146253338e+001 1.9e-009 0.92 38 2.6e-006 3.0e-002 1.9e-004 1.00e+000 1.145518120e+001 1.146234958e+001 1.7e-009 0.97 39 2.3e-006 2.8e-002 1.7e-004 1.00e+000 1.145573227e+001 1.146218380e+001 1.6e-009 1.00 40 2.1e-006 2.6e-002 1.5e-004 1.00e+000 1.145622801e+001 1.146203437e+001 1.4e-009 1.03 41 1.9e-006 2.4e-002 1.4e-004 1.00e+000 1.145667400e+001 1.146189965e+001 1.3e-009 1.08 42 1.7e-006 2.2e-002 1.2e-004 1.00e+000 1.145707519e+001 1.146177845e+001 1.1e-009 1.11 43 1.5e-006 2.1e-002 1.1e-004 1.00e+000 1.145743621e+001 1.146166905e+001 1.0e-009 1.14 44 1.4e-006 1.9e-002 1.0e-004 1.00e+000 1.145776101e+001 1.146157063e+001 9.3e-010 1.17 45 1.2e-006 1.8e-002 9.0e-005 1.00e+000 1.145805327e+001 1.146148192e+001 8.4e-010 1.20 46 1.1e-006 1.7e-002 8.1e-005 1.00e+000 1.145831622e+001 1.146140210e+001 7.5e-010 1.23 47 1.0e-006 1.6e-002 7.3e-005 9.99e-001 1.145855284e+001 1.146133023e+001 6.8e-010 1.26 48 9.0e-007 1.5e-002 6.6e-005 1.00e+000 1.145876578e+001 1.146126543e+001 6.1e-010 1.29 49 8.1e-007 1.4e-002 5.9e-005 9.99e-001 1.145895737e+001 1.146120718e+001 5.5e-010 1.33 50 7.3e-007 1.4e-002 5.3e-005 1.00e+000 1.145912983e+001 1.146115459e+001 4.9e-010 1.37 51 6.6e-007 1.3e-002 4.8e-005 1.00e+000 1.145928504e+001 1.146110721e+001 4.4e-010 1.40 52 2.3e-007 4.5e-003 1.7e-005 1.00e+000 1.146019580e+001 1.146082888e+001 1.5e-010 1.44 53 2.1e-007 4.0e-003 1.5e-005 1.00e+000 1.146024512e+001 1.146081423e+001 1.4e-010 1.47 54 7.2e-008 1.4e-003 5.2e-006 1.02e+000 1.146052973e+001 1.146072495e+001 4.8e-011 1.50 55 6.5e-008 1.3e-003 4.7e-006 9.79e-001 1.146054487e+001 1.146072074e+001 4.3e-011 1.53 56 5.9e-008 1.1e-003 4.2e-006 9.96e-001 1.146055844e+001 1.146071676e+001 3.9e-011 1.56 57 3.8e-008 1.2e-004 4.6e-007 8.82e-001 1.146067127e+001 1.146068972e+001 6.2e-012 1.59 58 2.9e-008 1.1e-004 4.1e-007 1.18e+000 1.146067271e+001 1.146068720e+001 6.0e-012 1.62 59 6.4e-009 1.7e-005 6.4e-008 1.09e+000 1.146067914e+001 1.146068119e+001 6.9e-013 1.65 Interior-point optimizer terminated. Time: 1.65. Optimizer terminated. Time: 1.67 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1460679142e+001 Viol. con: 1e-007 var: 0e+000 Dual. obj: 1.1460681192e+001 Viol. con: 0e+000 var: 1e-004 * End solution on dual form. * Transforming to primal solution. Solving took 1.7 seconds. result packing took 17% of solve time solution checking took 6.9% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Windows/64-X86 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1014 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.05 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.05 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.03 Factor - nonzeros before factor : 1.67e+004 after factor : 1.73e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289769222e+005 2.000000000e+000 1.0e+000 0.09 1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.266632853e+005 3.780424713e+000 4.6e-001 0.16 2 3.9e+002 5.0e+002 2.2e+004 -9.34e-001 -1.196648005e+005 1.164414827e+001 1.7e-001 0.17 3 2.8e+002 3.6e+002 1.6e+004 -8.25e-001 -1.157601409e+005 9.424063264e+001 1.2e-001 0.22 4 2.8e+002 3.6e+002 1.6e+004 -7.56e-001 -1.124497507e+005 2.795436247e+003 1.2e-001 0.27 5 8.0e+001 1.0e+002 4.5e+003 -7.46e-001 -7.580605879e+004 1.036154520e+004 3.5e-002 0.31 6 3.8e+001 5.0e+001 2.1e+003 -2.19e-001 -4.755669149e+004 1.111422426e+004 1.7e-002 0.36 7 2.1e+001 2.8e+001 1.2e+003 2.66e-001 -3.065191202e+004 7.195500862e+003 9.5e-003 0.39 8 9.6e+000 1.2e+001 5.4e+002 5.71e-001 -1.516646059e+004 3.841949798e+003 4.3e-003 0.44 9 4.1e+000 5.4e+000 2.3e+002 8.22e-001 -6.503657360e+003 2.072298342e+003 1.8e-003 0.47 10 1.9e+000 2.5e+000 1.1e+002 9.42e-001 -2.904824117e+003 1.164121984e+003 8.6e-004 0.52 11 1.3e+000 1.7e+000 7.5e+001 9.84e-001 -2.003999318e+003 8.081788704e+002 6.0e-004 0.56 12 8.8e-001 1.2e+000 5.0e+001 9.85e-001 -1.329416768e+003 5.561234239e+002 4.0e-004 0.59 13 6.8e-001 9.9e-001 3.8e+001 9.65e-001 -1.034611341e+003 4.305179491e+002 3.1e-004 0.64 14 2.9e-001 4.3e-001 1.7e+001 9.93e-001 -4.388193257e+002 1.991806486e+002 1.3e-004 0.67 15 1.3e-001 2.1e-001 7.6e+000 9.99e-001 -1.950471578e+002 9.656014319e+001 6.1e-005 0.72 16 4.2e-002 1.4e-001 2.5e+000 1.00e+000 -5.840119186e+001 3.622491374e+001 2.0e-005 0.76 17 3.5e-002 1.2e-001 2.1e+000 9.99e-001 -4.674888316e+001 3.160450650e+001 1.7e-005 0.80 18 1.9e-002 8.6e-002 1.1e+000 1.00e+000 -2.173553191e+001 2.047958428e+001 9.1e-006 0.83 19 1.1e-002 6.3e-002 6.5e-001 1.02e+000 -7.730492573e+000 1.647787226e+001 5.3e-006 0.86 20 3.6e-003 6.4e-002 2.2e-001 1.03e+000 5.273443871e+000 1.329837093e+001 1.8e-006 0.89 21 1.9e-003 5.2e-002 1.2e-001 1.00e+000 7.991887628e+000 1.233557385e+001 9.8e-007 0.92 22 5.5e-004 7.9e-002 3.6e-002 9.78e-001 1.030222160e+001 1.165622808e+001 3.1e-007 0.95 23 1.8e-004 7.8e-002 1.2e-002 9.66e-001 1.098188331e+001 1.144935755e+001 1.1e-007 0.98 24 8.8e-005 6.4e-002 6.2e-003 9.80e-001 1.116137467e+001 1.139881062e+001 5.6e-008 1.01 25 4.0e-005 6.1e-002 2.9e-003 9.90e-001 1.126322128e+001 1.137452009e+001 2.6e-008 1.04 26 3.6e-005 5.6e-002 2.6e-003 9.96e-001 1.127469414e+001 1.137490510e+001 2.4e-008 1.08 27 3.3e-005 5.1e-002 2.3e-003 9.96e-001 1.128254845e+001 1.137276235e+001 2.1e-008 1.12 28 3.0e-005 4.7e-002 2.1e-003 9.97e-001 1.128973936e+001 1.137095566e+001 1.9e-008 1.15 29 2.7e-005 4.3e-002 1.9e-003 9.97e-001 1.129617531e+001 1.136928902e+001 1.7e-008 1.19 30 2.4e-005 3.9e-002 1.7e-003 9.97e-001 1.130195095e+001 1.136776899e+001 1.6e-008 1.22 31 2.2e-005 3.6e-002 1.5e-003 9.98e-001 1.130713428e+001 1.136638343e+001 1.4e-008 1.25 32 1.9e-005 3.3e-002 1.4e-003 9.98e-001 1.131178740e+001 1.136512226e+001 1.3e-008 1.28 33 1.7e-005 3.1e-002 1.2e-003 9.98e-001 1.131596541e+001 1.136397550e+001 1.1e-008 1.31 34 1.6e-005 2.8e-002 1.1e-003 9.98e-001 1.131971755e+001 1.136293378e+001 1.0e-008 1.34 35 1.4e-005 2.6e-002 1.0e-003 9.98e-001 1.132308785e+001 1.136198822e+001 9.2e-009 1.37 36 1.3e-005 2.4e-002 9.1e-004 9.99e-001 1.132611572e+001 1.136113083e+001 8.3e-009 1.40 37 1.1e-005 2.2e-002 8.2e-004 9.99e-001 1.132883637e+001 1.136035387e+001 7.5e-009 1.44 38 1.0e-005 2.1e-002 7.4e-004 9.99e-001 1.133128136e+001 1.135965032e+001 6.7e-009 1.48 39 9.3e-006 2.0e-002 6.6e-004 9.99e-001 1.133347892e+001 1.135901367e+001 6.1e-009 1.51 40 8.3e-006 1.8e-002 6.0e-004 9.99e-001 1.133545432e+001 1.135843779e+001 5.5e-009 1.54 41 7.5e-006 1.7e-002 5.4e-004 9.99e-001 1.133723023e+001 1.135791718e+001 4.9e-009 1.61 42 6.8e-006 1.6e-002 4.8e-004 9.99e-001 1.133882692e+001 1.135744661e+001 4.4e-009 1.64 43 6.1e-006 1.5e-002 4.3e-004 9.99e-001 1.134026260e+001 1.135702153e+001 4.0e-009 1.69 44 5.5e-006 1.4e-002 3.9e-004 9.99e-001 1.134155354e+001 1.135663763e+001 3.6e-009 1.72 45 4.9e-006 1.4e-002 3.5e-004 9.99e-001 1.134271439e+001 1.135629093e+001 3.2e-009 1.75 46 4.4e-006 1.3e-002 3.2e-004 1.00e+000 1.134375832e+001 1.135597785e+001 2.9e-009 1.79 47 4.0e-006 1.2e-002 2.8e-004 1.00e+000 1.134469712e+001 1.135569527e+001 2.6e-009 1.83 48 3.6e-006 1.2e-002 2.6e-004 9.99e-001 1.134554143e+001 1.135544029e+001 2.3e-009 1.87 49 3.2e-006 1.1e-002 2.3e-004 1.00e+000 1.134630083e+001 1.135521016e+001 2.1e-009 1.90 50 2.9e-006 1.1e-002 2.1e-004 1.00e+000 1.134698391e+001 1.135500263e+001 1.9e-009 1.93 51 2.6e-006 1.1e-002 1.9e-004 1.00e+000 1.134759839e+001 1.135481548e+001 1.7e-009 1.98 52 2.4e-006 1.0e-002 1.7e-004 1.00e+000 1.134815121e+001 1.135464683e+001 1.5e-009 2.01 53 2.1e-006 9.9e-003 1.5e-004 1.00e+000 1.134864860e+001 1.135449482e+001 1.4e-009 2.04 54 1.9e-006 9.6e-003 1.4e-004 1.00e+000 1.134909615e+001 1.135435789e+001 1.2e-009 2.08 55 1.7e-006 9.4e-003 1.2e-004 1.00e+000 1.134949886e+001 1.135423461e+001 1.1e-009 2.11 56 1.5e-006 9.1e-003 1.1e-004 1.00e+000 1.134986127e+001 1.135412355e+001 1.0e-009 2.14 57 1.4e-006 8.9e-003 9.9e-005 1.00e+000 1.135018742e+001 1.135402355e+001 9.1e-010 2.17 58 1.3e-006 8.7e-003 8.9e-005 1.00e+000 1.135048095e+001 1.135393347e+001 8.2e-010 2.20 59 1.1e-006 8.6e-003 8.0e-005 1.00e+000 1.135074510e+001 1.135385246e+001 7.4e-010 2.25 60 1.0e-006 8.4e-003 7.2e-005 1.00e+000 1.135098286e+001 1.135377949e+001 6.6e-010 2.26 61 9.1e-007 8.3e-003 6.5e-005 1.00e+000 1.135119682e+001 1.135371386e+001 6.0e-010 2.29 62 8.2e-007 8.1e-003 5.9e-005 1.00e+000 1.135138941e+001 1.135365479e+001 5.4e-010 2.32 63 7.4e-007 8.0e-003 5.3e-005 1.00e+000 1.135156273e+001 1.135360165e+001 4.8e-010 2.36 64 6.6e-007 7.9e-003 4.8e-005 1.00e+000 1.135171876e+001 1.135355377e+001 4.4e-010 2.37 65 6.0e-007 7.8e-003 4.3e-005 1.00e+000 1.135185917e+001 1.135351071e+001 3.9e-010 2.40 66 5.4e-007 7.8e-003 3.8e-005 1.00e+000 1.135198557e+001 1.135347191e+001 3.5e-010 2.43 67 4.8e-007 7.7e-003 3.5e-005 9.99e-001 1.135209930e+001 1.135343709e+001 3.2e-010 2.45 68 4.4e-007 7.6e-003 3.1e-005 9.99e-001 1.135220167e+001 1.135340573e+001 2.9e-010 2.46 69 3.9e-007 7.5e-003 2.8e-005 1.00e+000 1.135229382e+001 1.135337747e+001 2.6e-010 2.48 70 3.5e-007 7.5e-003 2.5e-005 9.99e-001 1.135237675e+001 1.135335207e+001 2.3e-010 2.50 71 3.2e-007 7.4e-003 2.3e-005 1.00e+000 1.135245139e+001 1.135332919e+001 2.1e-010 2.53 72 2.9e-007 7.4e-003 2.0e-005 9.98e-001 1.135251855e+001 1.135330866e+001 1.9e-010 2.54 73 2.6e-007 7.3e-003 1.8e-005 1.00e+000 1.135257903e+001 1.135329007e+001 1.7e-010 2.56 74 2.3e-007 7.3e-003 1.7e-005 1.00e+000 1.135263367e+001 1.135327326e+001 1.5e-010 2.57 75 2.1e-007 7.3e-003 1.5e-005 9.99e-001 1.135268261e+001 1.135325827e+001 1.4e-010 2.59 76 1.9e-007 7.2e-003 1.3e-005 1.00e+000 1.135272668e+001 1.135324475e+001 1.2e-010 2.62 77 1.7e-007 7.2e-003 1.2e-005 9.98e-001 1.135276632e+001 1.135323264e+001 1.1e-010 2.65 78 1.5e-007 7.2e-003 1.1e-005 9.98e-001 1.135280199e+001 1.135322172e+001 1.0e-010 2.68 79 1.4e-007 7.2e-003 9.8e-006 9.98e-001 1.135283410e+001 1.135321190e+001 9.0e-011 2.71 80 1.2e-007 6.4e-003 8.8e-006 1.01e+000 1.135286356e+001 1.135320278e+001 8.1e-011 2.73 81 1.1e-007 5.8e-003 7.9e-006 1.00e+000 1.135288952e+001 1.135319483e+001 7.3e-011 2.76 82 1.0e-007 5.2e-003 7.1e-006 1.00e+000 1.135291289e+001 1.135318766e+001 6.5e-011 2.79 83 9.0e-008 4.7e-003 6.4e-006 1.00e+000 1.135293392e+001 1.135318119e+001 5.9e-011 2.82 84 8.1e-008 4.2e-003 5.8e-006 9.96e-001 1.135295283e+001 1.135317542e+001 5.3e-011 2.86 85 7.3e-008 3.8e-003 5.2e-006 1.00e+000 1.135296986e+001 1.135317019e+001 4.8e-011 2.87 86 6.5e-008 3.4e-003 4.7e-006 9.99e-001 1.135298518e+001 1.135316549e+001 4.3e-011 2.90 87 5.9e-008 3.1e-003 4.2e-006 9.94e-001 1.135299896e+001 1.135316129e+001 3.9e-011 2.93 88 5.3e-008 2.8e-003 3.8e-006 1.01e+000 1.135301181e+001 1.135315729e+001 3.5e-011 2.96 89 4.8e-008 2.5e-003 3.4e-006 1.00e+000 1.135302294e+001 1.135315387e+001 3.1e-011 2.98 90 4.3e-008 2.2e-003 3.1e-006 1.00e+000 1.135303296e+001 1.135315079e+001 2.8e-011 3.01 91 3.9e-008 2.0e-003 2.8e-006 9.94e-001 1.135304197e+001 1.135314805e+001 2.5e-011 3.04 92 3.5e-008 1.8e-003 2.5e-006 1.01e+000 1.135305037e+001 1.135314543e+001 2.3e-011 3.07 93 3.1e-008 1.6e-003 2.2e-006 1.01e+000 1.135305783e+001 1.135314312e+001 2.1e-011 3.10 94 2.8e-008 1.5e-003 2.0e-006 9.83e-001 1.135306434e+001 1.135314116e+001 1.9e-011 3.14 95 2.5e-008 1.3e-003 1.8e-006 9.98e-001 1.135307021e+001 1.135313936e+001 1.7e-011 3.17 96 2.3e-008 1.2e-003 1.6e-006 9.82e-001 1.135307549e+001 1.135313777e+001 1.5e-011 3.18 97 2.1e-008 1.1e-003 1.5e-006 9.71e-001 1.135308023e+001 1.135313636e+001 1.4e-011 3.21 98 1.9e-008 9.7e-004 1.3e-006 9.95e-001 1.135308451e+001 1.135313504e+001 1.2e-011 3.25 99 1.7e-008 8.7e-004 1.2e-006 9.89e-001 1.135308836e+001 1.135313386e+001 1.1e-011 3.28 100 1.5e-008 7.8e-004 1.1e-006 9.94e-001 1.135309182e+001 1.135313279e+001 9.9e-012 3.29 101 1.4e-008 7.0e-004 9.6e-007 1.04e+000 1.135309554e+001 1.135313157e+001 9.1e-012 3.32 102 2.6e-009 7.3e-005 1.0e-007 9.79e-001 1.135312032e+001 1.135312411e+001 1.0e-012 3.35 103 3.1e-010 5.1e-006 7.0e-009 1.03e+000 1.135312284e+001 1.135312310e+001 5.9e-014 3.38 Interior-point optimizer terminated. Time: 3.38. Optimizer terminated. Time: 3.40 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1353122842e+001 Viol. con: 5e-009 var: 0e+000 Dual. obj: 1.1353123098e+001 Viol. con: 0e+000 var: 4e-005 * End solution on dual form. * Transforming to primal solution. Solving took 3.44 seconds. result packing took 7.9% of solve time solution checking took 2.1% of solve time Using solver 'mosek' Solving for 1899 variables. Number of Hessian non-zeros: 1953 * Solving exponential optimization problem on dual form. * * The following log information refers to the solution of the dual problem. * Computer Platform : Windows/64-X86 Problem Name : Objective sense : max Type : GECO (general convex optimization problem) Constraints : 1900 Cones : 0 Scalar variables : 6471 Matrix variables : 0 Integer variables : 0 Optimizer started. Interior-point optimizer started. Presolve started. Linear dependency checker started. Linear dependency checker terminated. Eliminator started. Total number of eliminations : 1013 Eliminator terminated. Eliminator started. Total number of eliminations : 1023 Eliminator terminated. Eliminator - tries : 2 time : 0.00 Eliminator - elim's : 1023 Lin. dep. - tries : 1 time : 0.00 Lin. dep. - number : 0 Presolve terminated. Time: 0.01 Matrix reordering started. Local matrix reordering started. Local matrix reordering terminated. Matrix reordering terminated. Optimizer - threads : 6 Optimizer - solved problem : the primal Optimizer - Constraints : 830 Optimizer - Cones : 0 Optimizer - Scalar variables : 3579 conic : 0 Optimizer - Semi-definite variables: 0 scalarized : 0 Factor - setup time : 0.03 dense det. time : 0.00 Factor - ML order time : 0.00 GP order time : 0.01 Factor - nonzeros before factor : 1.67e+004 after factor : 1.73e+005 Factor - dense dim. : 0 flops : 0.00e+000 Factor - GP saved nzs : 0 GP saved flops : 0.00e+000 ITE PFEAS DFEAS GFEAS PRSTATUS POBJ DOBJ MU TIME 0 2.3e+003 3.0e+003 1.3e+005 0.00e+000 -1.289733434e+005 2.000000000e+000 1.0e+000 0.05 1 1.1e+003 1.4e+003 5.9e+004 -9.71e-001 -1.266535155e+005 3.775373334e+000 4.6e-001 0.09 2 3.8e+002 4.9e+002 2.1e+004 -9.34e-001 -1.194617156e+005 1.183435194e+001 1.7e-001 0.14 3 2.8e+002 3.6e+002 1.6e+004 -8.22e-001 -1.157203455e+005 1.058333166e+002 1.2e-001 0.17 4 2.8e+002 3.6e+002 1.5e+004 -7.56e-001 -1.123748408e+005 2.767546129e+003 1.2e-001 0.22 5 7.9e+001 1.0e+002 4.4e+003 -7.45e-001 -7.538890048e+004 1.048273349e+004 3.5e-002 0.27 6 3.7e+001 4.8e+001 2.1e+003 -2.13e-001 -4.621988935e+004 1.115536324e+004 1.6e-002 0.30 7 2.0e+001 2.6e+001 1.1e+003 2.89e-001 -2.885876816e+004 7.126464190e+003 8.9e-003 0.34 8 9.5e+000 1.2e+001 5.3e+002 6.02e-001 -1.497254698e+004 3.847953955e+003 4.2e-003 0.39 9 4.4e+000 5.6e+000 2.4e+002 8.27e-001 -6.851478072e+003 2.133840683e+003 1.9e-003 0.42 10 1.5e+000 2.0e+000 8.6e+001 9.39e-001 -2.274862815e+003 9.554998797e+002 6.9e-004 0.47 11 1.1e+000 1.5e+000 6.4e+001 9.89e-001 -1.707016226e+003 7.086246389e+002 5.1e-004 0.50 12 7.3e-001 9.7e-001 4.1e+001 9.84e-001 -1.107953425e+003 4.689637162e+002 3.3e-004 0.53 13 6.0e-001 7.9e-001 3.4e+001 9.85e-001 -8.900754559e+002 3.930801434e+002 2.7e-004 0.56 14 2.2e-001 3.0e-001 1.2e+001 9.87e-001 -3.293840236e+002 1.438009456e+002 1.0e-004 0.61 15 9.1e-002 1.4e-001 5.3e+000 1.01e+000 -1.321443716e+002 6.830671160e+001 4.3e-005 0.64 16 3.6e-002 9.9e-002 2.1e+000 1.00e+000 -4.896880973e+001 3.135904594e+001 1.7e-005 0.67 17 2.9e-002 8.4e-002 1.7e+000 9.97e-001 -3.803916802e+001 2.780242537e+001 1.4e-005 0.70 18 1.8e-002 6.6e-002 1.1e+000 1.01e+000 -1.986393079e+001 2.050583856e+001 8.7e-006 0.73 19 1.6e-002 5.9e-002 9.4e-001 1.02e+000 -1.584462832e+001 1.949843457e+001 7.7e-006 0.78 20 5.7e-003 6.7e-002 3.4e-001 1.02e+000 1.623673030e+000 1.417728764e+001 2.8e-006 0.81 21 1.9e-003 7.7e-002 1.2e-001 1.02e+000 7.977777524e+000 1.238204092e+001 1.0e-006 0.84 22 1.4e-003 5.8e-002 8.7e-002 9.67e-001 8.837182080e+000 1.205720045e+001 7.5e-007 0.89 23 4.9e-004 6.7e-002 3.2e-002 9.60e-001 1.037811769e+001 1.161136962e+001 2.9e-007 0.92 24 2.0e-004 6.1e-002 1.3e-002 9.57e-001 1.091882551e+001 1.143305557e+001 1.2e-007 0.95 25 1.8e-004 5.5e-002 1.2e-002 9.76e-001 1.095735758e+001 1.141997157e+001 1.1e-007 0.98 26 1.6e-004 5.0e-002 1.1e-002 9.74e-001 1.099290464e+001 1.140980212e+001 9.7e-008 1.00 27 1.4e-004 4.6e-002 9.7e-003 9.75e-001 1.102762256e+001 1.140338684e+001 8.8e-008 1.04 28 1.3e-004 4.2e-002 8.8e-003 9.77e-001 1.105899544e+001 1.139766315e+001 7.9e-008 1.08 29 1.2e-004 3.9e-002 7.9e-003 9.79e-001 1.108724167e+001 1.139244396e+001 7.1e-008 1.09 30 1.0e-004 3.5e-002 7.1e-003 9.81e-001 1.111261377e+001 1.138762903e+001 6.4e-008 1.12 31 9.4e-005 3.3e-002 6.4e-003 9.83e-001 1.113539514e+001 1.138318499e+001 5.8e-008 1.14 32 8.5e-005 3.0e-002 5.8e-003 9.84e-001 1.115584400e+001 1.137908338e+001 5.2e-008 1.15 33 7.6e-005 2.8e-002 5.2e-003 9.86e-001 1.117419490e+001 1.137529933e+001 4.7e-008 1.17 34 6.9e-005 2.6e-002 4.7e-003 9.87e-001 1.119065991e+001 1.137180987e+001 4.2e-008 1.19 35 6.2e-005 2.4e-002 4.2e-003 9.88e-001 1.120543125e+001 1.136859483e+001 3.8e-008 1.20 36 5.6e-005 2.2e-002 3.8e-003 9.89e-001 1.121868219e+001 1.136563543e+001 3.4e-008 1.23 37 5.0e-005 2.1e-002 3.4e-003 9.90e-001 1.123056883e+001 1.136291396e+001 3.1e-008 1.25 38 4.5e-005 1.9e-002 3.1e-003 9.91e-001 1.124123186e+001 1.136041419e+001 2.8e-008 1.26 39 4.1e-005 1.8e-002 2.8e-003 9.92e-001 1.125079744e+001 1.135812043e+001 2.5e-008 1.28 40 3.7e-005 1.7e-002 2.5e-003 9.93e-001 1.125937874e+001 1.135601774e+001 2.2e-008 1.29 41 3.3e-005 1.6e-002 2.2e-003 9.94e-001 1.126707737e+001 1.135409202e+001 2.0e-008 1.31 42 3.0e-005 1.5e-002 2.0e-003 9.94e-001 1.127398449e+001 1.135233006e+001 1.8e-008 1.34 43 2.7e-005 1.4e-002 1.8e-003 9.95e-001 1.128018197e+001 1.135071954e+001 1.6e-008 1.36 44 2.4e-005 1.4e-002 1.6e-003 9.95e-001 1.128574346e+001 1.134924898e+001 1.5e-008 1.37 45 2.2e-005 1.3e-002 1.5e-003 9.96e-001 1.129073513e+001 1.134790784e+001 1.3e-008 1.39 46 1.9e-005 1.2e-002 1.3e-003 9.96e-001 1.129521618e+001 1.134668603e+001 1.2e-008 1.40 47 1.7e-005 1.2e-002 1.2e-003 9.97e-001 1.129923958e+001 1.134557428e+001 1.1e-008 1.42 48 1.6e-005 1.1e-002 1.1e-003 9.97e-001 1.130285261e+001 1.134456351e+001 9.6e-009 1.45 49 1.4e-005 1.1e-002 9.6e-004 9.97e-001 1.130609765e+001 1.134364532e+001 8.7e-009 1.47 50 1.3e-005 1.1e-002 8.7e-004 9.98e-001 1.130901266e+001 1.134281196e+001 7.8e-009 1.48 51 1.1e-005 1.0e-002 7.8e-004 9.98e-001 1.131163158e+001 1.134205617e+001 7.0e-009 1.50 52 1.0e-005 1.0e-002 7.0e-004 9.98e-001 1.131398480e+001 1.134137119e+001 6.3e-009 1.51 53 9.3e-006 9.7e-003 6.3e-004 9.98e-001 1.131609954e+001 1.134075082e+001 5.7e-009 1.53 54 8.4e-006 9.4e-003 5.7e-004 9.98e-001 1.131800016e+001 1.134018914e+001 5.1e-009 1.54 55 7.5e-006 9.2e-003 5.1e-004 9.99e-001 1.131970853e+001 1.133968094e+001 4.6e-009 1.56 56 6.8e-006 9.0e-003 4.6e-004 9.99e-001 1.132124420e+001 1.133922120e+001 4.2e-009 1.59 57 6.1e-006 8.8e-003 4.1e-004 9.99e-001 1.132262472e+001 1.133880555e+001 3.7e-009 1.61 58 5.5e-006 8.6e-003 3.7e-004 9.99e-001 1.132386580e+001 1.133842978e+001 3.4e-009 1.62 59 4.9e-006 8.5e-003 3.4e-004 9.99e-001 1.132498160e+001 1.133809018e+001 3.0e-009 1.64 60 4.4e-006 8.3e-003 3.0e-004 9.99e-001 1.132598478e+001 1.133778335e+001 2.7e-009 1.65 61 4.0e-006 8.2e-003 2.7e-004 9.99e-001 1.132688676e+001 1.133750618e+001 2.5e-009 1.67 62 3.6e-006 8.1e-003 2.4e-004 1.00e+000 1.132769782e+001 1.133725580e+001 2.2e-009 1.70 63 3.2e-006 8.0e-003 2.2e-004 1.00e+000 1.132842717e+001 1.133702979e+001 2.0e-009 1.72 64 2.9e-006 7.9e-003 2.0e-004 9.99e-001 1.132908310e+001 1.133682585e+001 1.8e-009 1.73 65 2.6e-006 7.8e-003 1.8e-004 1.00e+000 1.132967307e+001 1.133664185e+001 1.6e-009 1.75 66 2.4e-006 7.7e-003 1.6e-004 1.00e+000 1.133020376e+001 1.133647591e+001 1.4e-009 1.76 67 2.1e-006 7.7e-003 1.4e-004 1.00e+000 1.133068117e+001 1.133632633e+001 1.3e-009 1.78 68 1.9e-006 7.6e-003 1.3e-004 1.00e+000 1.133111067e+001 1.133619149e+001 1.2e-009 1.79 69 1.7e-006 7.5e-003 1.2e-004 1.00e+000 1.133149711e+001 1.133606997e+001 1.1e-009 1.81 70 1.6e-006 7.5e-003 1.1e-004 1.00e+000 1.133184482e+001 1.133596047e+001 9.5e-010 1.84 71 1.4e-006 7.4e-003 9.5e-005 1.00e+000 1.133215768e+001 1.133586184e+001 8.6e-010 1.86 72 1.3e-006 7.4e-003 8.5e-005 1.00e+000 1.133243919e+001 1.133577302e+001 7.7e-010 1.87 73 1.1e-006 7.4e-003 7.7e-005 1.00e+000 1.133269253e+001 1.133569299e+001 6.9e-010 1.89 74 1.0e-006 7.3e-003 6.9e-005 1.00e+000 1.133292049e+001 1.133562096e+001 6.2e-010 1.90 75 9.2e-007 7.3e-003 6.2e-005 1.00e+000 1.133312563e+001 1.133555608e+001 5.6e-010 1.92 76 8.2e-007 7.2e-003 5.6e-005 1.00e+000 1.133331024e+001 1.133549766e+001 5.1e-010 1.93 77 7.4e-007 7.2e-003 5.0e-005 1.00e+000 1.133347637e+001 1.133544508e+001 4.5e-010 1.95 78 6.7e-007 7.2e-003 4.5e-005 1.00e+000 1.133362587e+001 1.133539772e+001 4.1e-010 1.98 79 6.0e-007 7.2e-003 4.1e-005 1.00e+000 1.133376043e+001 1.133535504e+001 3.7e-010 2.00 80 5.4e-007 7.1e-003 3.7e-005 1.00e+000 1.133388150e+001 1.133531669e+001 3.3e-010 2.01 81 4.9e-007 7.1e-003 3.3e-005 1.00e+000 1.133399046e+001 1.133528214e+001 3.0e-010 2.03 82 4.4e-007 7.1e-003 3.0e-005 1.00e+000 1.133408851e+001 1.133525105e+001 2.7e-010 2.04 83 3.9e-007 7.1e-003 2.7e-005 1.00e+000 1.133417676e+001 1.133522307e+001 2.4e-010 2.06 84 3.5e-007 7.1e-003 2.4e-005 1.00e+000 1.133425617e+001 1.133519785e+001 2.2e-010 2.07 85 3.2e-007 7.0e-003 2.2e-005 1.00e+000 1.133432764e+001 1.133517518e+001 2.0e-010 2.09 86 2.9e-007 7.0e-003 2.0e-005 1.00e+000 1.133439196e+001 1.133515474e+001 1.8e-010 2.12 87 2.6e-007 7.0e-003 1.8e-005 9.99e-001 1.133444983e+001 1.133513637e+001 1.6e-010 2.14 88 2.3e-007 7.0e-003 1.6e-005 9.99e-001 1.133450191e+001 1.133511983e+001 1.4e-010 2.15 89 2.1e-007 7.0e-003 1.4e-005 1.00e+000 1.133454880e+001 1.133510488e+001 1.3e-010 2.17 90 1.9e-007 7.0e-003 1.3e-005 1.00e+000 1.133459099e+001 1.133509145e+001 1.2e-010 2.18 91 1.7e-007 7.0e-003 1.2e-005 1.00e+000 1.133462896e+001 1.133507936e+001 1.0e-010 2.20 92 1.5e-007 7.0e-003 1.0e-005 9.99e-001 1.133466312e+001 1.133506850e+001 9.4e-011 2.21 93 1.4e-007 6.9e-003 9.3e-006 9.99e-001 1.133469386e+001 1.133505872e+001 8.4e-011 2.23 94 1.2e-007 6.9e-003 8.4e-006 1.00e+000 1.133472159e+001 1.133504986e+001 7.6e-011 2.26 95 1.1e-007 6.9e-003 7.6e-006 1.00e+000 1.133474648e+001 1.133504194e+001 6.8e-011 2.28 96 1.0e-007 6.2e-003 6.8e-006 1.00e+000 1.133476919e+001 1.133503466e+001 6.2e-011 2.29 97 9.0e-008 5.6e-003 6.1e-006 1.00e+000 1.133478932e+001 1.133502824e+001 5.5e-011 2.31 98 8.1e-008 5.1e-003 5.5e-006 9.96e-001 1.133480743e+001 1.133502249e+001 5.0e-011 2.32 99 7.3e-008 4.5e-003 5.0e-006 1.00e+000 1.133482373e+001 1.133501729e+001 4.5e-011 2.34 100 6.6e-008 4.1e-003 4.5e-006 9.99e-001 1.133483841e+001 1.133501262e+001 4.0e-011 2.36 101 5.9e-008 3.7e-003 4.0e-006 1.00e+000 1.133485173e+001 1.133500834e+001 3.6e-011 2.37 102 5.3e-008 3.3e-003 3.6e-006 1.00e+000 1.133486360e+001 1.133500456e+001 3.3e-011 2.40 103 4.8e-008 3.0e-003 3.3e-006 1.01e+000 1.133487457e+001 1.133500102e+001 3.0e-011 2.42 104 4.3e-008 2.7e-003 2.9e-006 1.00e+000 1.133488422e+001 1.133499793e+001 2.7e-011 2.43 105 3.9e-008 2.4e-003 2.6e-006 1.00e+000 1.133489284e+001 1.133499519e+001 2.4e-011 2.45 106 3.5e-008 2.2e-003 2.4e-006 1.01e+000 1.133490077e+001 1.133499263e+001 2.2e-011 2.46 107 3.1e-008 2.0e-003 2.1e-006 1.00e+000 1.133490781e+001 1.133499038e+001 1.9e-011 2.48 108 2.8e-008 1.8e-003 1.9e-006 1.01e+000 1.133491423e+001 1.133498831e+001 1.8e-011 2.50 109 2.5e-008 1.6e-003 1.7e-006 9.97e-001 1.133491985e+001 1.133498653e+001 1.6e-011 2.51 110 5.0e-009 3.0e-004 3.3e-007 9.91e-001 1.133496083e+001 1.133497360e+001 3.1e-012 2.54 111 1.6e-009 3.3e-005 3.6e-008 1.01e+000 1.133496932e+001 1.133497069e+001 3.2e-013 2.56 Interior-point optimizer terminated. Time: 2.56. Optimizer terminated. Time: 2.57 solsta = 1, prosta = 1 Interior-point solution summary Problem status : PRIMAL_AND_DUAL_FEASIBLE Solution status : OPTIMAL Primal. obj: 1.1334969324e+001 Viol. con: 3e-008 var: 0e+000 Dual. obj: 1.1334970693e+001 Viol. con: 0e+000 var: 2e-004 * End solution on dual form. * Transforming to primal solution. Solving took 2.61 seconds. result packing took 12% of solve time solution checking took 3.4% of solve time Solving took 6 GP solves and 27.1 seconds. 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 2418946.32587 force_pound * meter but the right hand side evaluated to 2375461.26787 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 32774.3879686 force_pound but the right hand side evaluated to 32399.9999959 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 2.21510116764 meter but the right hand side evaluated to 2.08160972236 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 1243582.25222 joule / kilogram but the right hand side evaluated to 1.56115364952 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 664761.501503 joule / kilogram but the right hand side evaluated to 0.667340277015 megajoule / kilogram (Allowable error: 0.1%, Actual error: 0.17%) Warning: Constraint [x_m_Mission/Aircraft/LandingGear [m]... >= x_{wing}_Mission/Aircraft/Fuselage [m]...] is not tight because the left hand side evaluated to 18.3998911495 meter but the right hand side evaluated to 16.3228871172 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 10.903624230788907 but the right hand side evaluated to 4.788856759192273 (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 10.019806158817136 but the right hand side evaluated to 4.788856741235013 (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 8.144908651915312 but the right hand side evaluated to 4.788856763572122 (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 18.3622317813 meter but the right hand side evaluated to 18.1377217947 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 18.3622317813 meter but the right hand side evaluated to 18.2420577969 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 0.29603376223427613 but the right hand side evaluated to 0.18973855343232612 (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 0.23301942810156007 but the right hand side evaluated to 0.17434617395003452 (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 7.563248370093851 but the right hand side evaluated to 4.730638127433166 (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 7.583098634684433 but the right hand side evaluated to 4.757850799214973 (Allowable error: 0.1%, Actual error: 37%) Solves with these variables bounded: value near lower bound: CruiseAlt_Mission value near upper bound: TotalTime_Mission, A_{tri}_Mission/Aircraft/Wing/WingNoStruct Running tests... ---------------------------------------------------------------------- . ---------------------------------------------------------------------- Ran 1 test in 35.026s OK Generating XML reports... Cloning into 'solar'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.23.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gpfit.git Cloning https://github.com/convexengineering/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-prw2t5 Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/convexengineering/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.0) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->gpfit==0.1) (2018.0.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->gpfit==0.1) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-8egqav\wheels\d5\94\ac\b1f68b07599181f26f4b9149a1a6d49dfc5cdbc65de1a14d12 Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/convexengineering/gassolar.git Cloning https://github.com/convexengineering/gassolar.git to c:\users\jenkins\appdata\local\temp\pip-req-build-9gugoh Requirement already satisfied (use --upgrade to upgrade): gassolar==0.0.0.0 from git+https://github.com/convexengineering/gassolar.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gassolar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from gassolar==0.0.0.0) (0.23.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from gassolar==0.0.0.0) (0.1) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->gassolar==0.0.0.0) (1.2.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas->gassolar==0.0.0.0) (2.6.1) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->gassolar==0.0.0.0) (2018.0.0) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas->gassolar==0.0.0.0) (1.11.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->gassolar==0.0.0.0) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-abuiib\wheels\fe\11\0a\2dde16df75c51194d20248ec9e30e88fc7200e9fc4664b032e Successfully built gassolar grin 1.2.1 requires argparse>=1.1, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\solar Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from solar==0.0.0.0) (0.7.0.0) Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (from solar==0.0.0.0) (0.23.0) Requirement already satisfied: gpfit in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages (from solar==0.0.0.0) (0.1) Requirement already satisfied: gpkitmodels in d:\jenkins\workspace\gplibrary_pr_models\mosek (from solar==0.0.0.0) (0.0.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->solar==0.0.0.0) (1.2.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas->solar==0.0.0.0) (2.6.1) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->solar==0.0.0.0) (2018.0.0) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas->solar==0.0.0.0) (1.11.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->solar==0.0.0.0) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-5ef6ie\wheels\9f\ae\a9\52e286ff9ea1428d6dd1e8c6df0d12b22c44363d9dcc1dd331 Successfully built solar grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: solar Successfully installed solar-0.0.0.0 adding test for 'solar/sens_chart.py' adding test for 'solar/season.py' adding test for 'solar/npod_trade.py' Beginning signomial solve. Solving took 5 GP solves and 2.22 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 0.8904 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 1632916.9408 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1259333.2946 but bound is 1000000.0000 Beginning signomial solve. Solving took 6 GP solves and 2.94 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1036204.4248 but bound is 600000.0000 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/TailAero.5_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1006645.3422 but bound is 1000000.0000 Beginning signomial solve. Solving took 7 GP solves and 4.03 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is above upper bound. Solution is 989673.4623 but bound is 600000.0000 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.4/TailAero.9_(0,), Re_Mission.2/Climb.2/AircraftDrag.4/TailAero.9 could cause inaccurate result because it is above upper bound. Solution is 1019678.5274 but bound is 1000000.0000 Beginning signomial solve. Solving took 6 GP solves and 4.2 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.6/WingAero.6_(0,), CL_Mission.3/Climb.3/AircraftDrag.6/WingAero.6 could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.6/WingAero.6_(0,), Re_Mission.3/Climb.3/AircraftDrag.6/WingAero.6 could cause inaccurate result because it is above upper bound. Solution is 976142.1407 but bound is 600000.0000 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.6/TailAero.13_(0,), Re_Mission.3/Climb.3/AircraftDrag.6/TailAero. could cause inaccurate result because it is above upper bound. Solution is 1042059.4014 but bound is 1000000.0000 Beginning signomial solve. Solving took 6 GP solves and 3.76 seconds. Warning: Variable [CL_Mission.4/Climb.4/AircraftDrag.8/WingAero.8_(0,), CL_Mission.4/Climb.4/AircraftDrag.8/WingAero.8 could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465 Warning: Variable [Re_Mission.4/Climb.4/AircraftDrag.8/WingAero.8_(0,), Re_Mission.4/Climb.4/AircraftDrag.8/WingAero.8 could cause inaccurate result because it is above upper bound. Solution is 1007400.4711 but bound is 600000.0000 Warning: Variable [Re_Mission.4/Climb.4/AircraftDrag.8/TailAero.17_(0,), Re_Mission.4/Climb.4/AircraftDrag.8/TailAero. could cause inaccurate result because it is above upper bound. Solution is 1092545.5044 but bound is 1000000.0000 Beginning signomial solve. Solving took 4 GP solves and 1.57 seconds. Warning: Variable [CL_Mission.5/Climb.5/AircraftDrag.10/WingAero.10_(0,), CL_Mission.5/Climb.5/AircraftDrag.10/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465 Warning: Variable [Re_Mission.5/Climb.5/AircraftDrag.10/WingAero.10_(0,), Re_Mission.5/Climb.5/AircraftDrag.10/WingAer could cause inaccurate result because it is above upper bound. Solution is 1119121.2013 but bound is 600000.0000 Beginning signomial solve. Solving took 5 GP solves and 1.84 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 0.8904 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 1632916.9407 but bound is 600000.0000 Warning: Variable [Re_Mission/Climb/AircraftDrag/TailAero.1_(0,), Re_Mission/Climb/AircraftDrag/TailAero.1_(1,), Re_Mi could cause inaccurate result because it is above upper bound. Solution is 1259333.2945 but bound is 1000000.0000 Beginning signomial solve. Solving took 6 GP solves and 4.07 seconds. Warning: Variable [CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), CL_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is below lower bound. Solution is 1.1135 but bound is 0.9465 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/WingAero.2 could cause inaccurate result because it is above upper bound. Solution is 1036204.4226 but bound is 600000.0000 Warning: Variable [Re_Mission.1/Climb.1/AircraftDrag.2/TailAero.5_(0,), Re_Mission.1/Climb.1/AircraftDrag.2/TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1006645.3412 but bound is 1000000.0000 Beginning signomial solve. Solving took 7 GP solves and 7.32 seconds. Warning: Variable [CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), CL_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is below lower bound. Solution is 1.1487 but bound is 0.9465 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4_(0,), Re_Mission.2/Climb.2/AircraftDrag.4/WingAero.4 could cause inaccurate result because it is above upper bound. Solution is 989673.4622 but bound is 600000.0000 Warning: Variable [Re_Mission.2/Climb.2/AircraftDrag.4/TailAero.9_(0,), Re_Mission.2/Climb.2/AircraftDrag.4/TailAero.9 could cause inaccurate result because it is above upper bound. Solution is 1019678.5273 but bound is 1000000.0000 Beginning signomial solve. Solving took 6 GP solves and 6.34 seconds. Warning: Variable [CL_Mission.3/Climb.3/AircraftDrag.6/WingAero.6_(0,), CL_Mission.3/Climb.3/AircraftDrag.6/WingAero.6 could cause inaccurate result because it is below lower bound. Solution is 1.1643 but bound is 0.9465 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.6/WingAero.6_(0,), Re_Mission.3/Climb.3/AircraftDrag.6/WingAero.6 could cause inaccurate result because it is above upper bound. Solution is 976142.1406 but bound is 600000.0000 Warning: Variable [Re_Mission.3/Climb.3/AircraftDrag.6/TailAero.13_(0,), Re_Mission.3/Climb.3/AircraftDrag.6/TailAero. could cause inaccurate result because it is above upper bound. Solution is 1042059.4014 but bound is 1000000.0000 Beginning signomial solve. Solving took 6 GP solves and 5.67 seconds. Warning: Variable [CL_Mission.4/Climb.4/AircraftDrag.8/WingAero.8_(0,), CL_Mission.4/Climb.4/AircraftDrag.8/WingAero.8 could cause inaccurate result because it is below lower bound. Solution is 1.1567 but bound is 0.9465 Warning: Variable [Re_Mission.4/Climb.4/AircraftDrag.8/WingAero.8_(0,), Re_Mission.4/Climb.4/AircraftDrag.8/WingAero.8 could cause inaccurate result because it is above upper bound. Solution is 1007400.4711 but bound is 600000.0000 Warning: Variable [Re_Mission.4/Climb.4/AircraftDrag.8/TailAero.17_(0,), Re_Mission.4/Climb.4/AircraftDrag.8/TailAero. could cause inaccurate result because it is above upper bound. Solution is 1092545.5044 but bound is 1000000.0000 Beginning signomial solve. Solving took 4 GP solves and 1.48 seconds. Warning: Variable [CL_Mission.5/Climb.5/AircraftDrag.10/WingAero.10_(0,), CL_Mission.5/Climb.5/AircraftDrag.10/WingAer could cause inaccurate result because it is below lower bound. Solution is 1.0536 but bound is 0.9465 Warning: Variable [Re_Mission.5/Climb.5/AircraftDrag.10/WingAero.10_(0,), Re_Mission.5/Climb.5/AircraftDrag.10/WingAer could cause inaccurate result because it is above upper bound. Solution is 1119121.2012 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.39 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 1.3227 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 671709.7362 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 4.84 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 1.2812 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 729183.6153 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 4.65 seconds. Allowing negative dual variable(s) as small as -3.427086457501172e-11. 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 1.2258 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 802959.5989 but bound is 600000.0000 Using solver 'mosek' Solving for 7672 variables. Solving took 2.15 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 1.2008 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 839122.5075 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.59 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 1.3227 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 671709.7472 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.41 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 1.2812 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 729183.6152 but bound is 600000.0000 Using solver 'mosek' Solving for 14852 variables. Solving took 5.56 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 1.2258 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 802959.5989 but bound is 600000.0000 Using solver 'mosek' Solving for 7672 variables. Solving took 3.33 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 1.2008 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 839122.5075 but bound is 600000.0000 Beginning signomial solve. Solving took 4 GP solves and 1.98 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 1.0536 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 1119121.2012 but bound is 600000.0000 Beginning signomial solve. Solving took 4 GP solves and 2.08 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 1.0536 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 1119121.2012 but bound is 600000.0000 Running tests... ---------------------------------------------------------------------- ..D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: overflow encountered in exp tau = np.exp(-0.175/costhsun) D:\jenkins\workspace\gplibrary_PR_Models\mosek\venv2_gpkit\lib\site-packages\gassolar\environment\solar_irradiance.py:40: RuntimeWarning: divide by zero encountered in divide tau = np.exp(-0.175/costhsun) .... ---------------------------------------------------------------------- Ran 6 tests in 558.270s OK Generating XML reports... Cloning into 'gplibrary'... Requirement already satisfied: pandas in d:\anaconda2\lib\site-packages (0.23.0) Requirement already satisfied: pytz>=2011k in d:\anaconda2\lib\site-packages (from pandas) (2017.3) Requirement already satisfied: python-dateutil>=2.5.0 in d:\anaconda2\lib\site-packages (from pandas) (2.6.1) Requirement already satisfied: numpy>=1.9.0 in d:\anaconda2\lib\site-packages (from pandas) (1.14.3) Requirement already satisfied: six>=1.5 in d:\anaconda2\lib\site-packages (from python-dateutil>=2.5.0->pandas) (1.11.0) grin 1.2.1 requires argparse>=1.1, which is not installed. Collecting git+https://github.com/hoburg/gpfit.git Cloning https://github.com/hoburg/gpfit.git to c:\users\jenkins\appdata\local\temp\pip-req-build-xg_cjy Requirement already satisfied (use --upgrade to upgrade): gpfit==0.1 from git+https://github.com/hoburg/gpfit.git in d:\jenkins\workspace\gplibrary_pr_models\mosek\venv2_gpkit\lib\site-packages Requirement already satisfied: numpy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpfit==0.1) (1.1.0) Requirement already satisfied: gpkit in d:\jenkins\workspace\gplibrary_pr_models\mosek\gpkit (from gpfit==0.1) (0.7.0.0) Requirement already satisfied: pint>=0.7 in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.8.1) Requirement already satisfied: ad in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.3.2) Requirement already satisfied: ctypesgen in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (0.post125) Requirement already satisfied: cvxopt in d:\anaconda2\lib\site-packages (from gpkit->gpfit==0.1) (1.2.0) Requirement already satisfied: mkl in d:\anaconda2\lib\site-packages (from cvxopt->gpkit->gpfit==0.1) (2018.0.0) Requirement already satisfied: intel-openmp==2018.0.0 in d:\anaconda2\lib\site-packages (from mkl->cvxopt->gpkit->gpfit==0.1) (2018.0.0) 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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-yrnls7\wheels\4d\4b\2e\9480645acbe8d32004b09b3732f616bbb2a9ee75e4526f058f Successfully built gpfit grin 1.2.1 requires argparse>=1.1, which is not installed. Processing d:\jenkins\workspace\gplibrary_pr_models\mosek\gplibrary Requirement already satisfied: numpy>=1.12 in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.14.3) Requirement already satisfied: scipy in d:\anaconda2\lib\site-packages (from gpkitmodels==0.0.0.0) (1.1.0) Requirement already satisfied: pint in d:\anaconda2\lib\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: c:\users\jenkins\appdata\local\temp\pip-ephem-wheel-cache-1ylzex\wheels\4a\da\60\bea5372bf288606a399bdc749979f532f5aff24f4c362a9887 Successfully built gpkitmodels grin 1.2.1 requires argparse>=1.1, which is not installed. Installing collected packages: gpkitmodels Found existing installation: gpkitmodels 0.0.0.0 Uninstalling gpkitmodels-0.0.0.0: Successfully uninstalled gpkitmodels-0.0.0.0 Successfully installed gpkitmodels-0.0.0.0 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 0.037 seconds. Using solver 'mosek_cli' Solving for 11 variables. Solving took 0.093 seconds. Using solver 'mosek' Solving for 9 variables. Solving took 0.021 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.024 seconds. Using solver 'mosek' Solving for 25 variables. Solving took 0.02 seconds. Beginning signomial solve. Solving took 16 GP solves and 2.64 seconds. Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006556021 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544371523 meter * revolutions_per_minute but the right hand side evaluated to 103.041409431 meter / second (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585925008 meter ** 2 / second ** 2 but the right hand side evaluated to 0.420573144949 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.003%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.31464503395 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629895187 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0048%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.168936438401 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931603966 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0639642380809 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639631379932 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0017%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356535436 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226354005884 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0011%) Using solver 'mosek_cli' Solving for 9 variables. Solving took 0.094 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.097 seconds. Using solver 'mosek_cli' Solving for 25 variables. Solving took 0.101 seconds. Beginning signomial solve. Solving took 16 GP solves and 4.89 seconds. Warning: Constraint [dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,) + dT_BladeElem... >= T_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp [lbf]...] is not tight because the left hand side evaluated to 100.006568341 force_pound but the right hand side evaluated to 100.0 force_pound (Allowable error: 0.0001%, Actual error: 0.0066%) Warning: Constraint [omega_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)*r_BladeElem... >= Wt_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,) + vt_BladeElem...] is not tight because the left hand side evaluated to 985.544539109 meter * revolutions_per_minute but the right hand side evaluated to 103.041408191 meter / second (Allowable error: 0.0001%, Actual error: 0.16%) Warning: Constraint [dQ_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [N*m]... >= B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement_...] is not tight because the left hand side evaluated to 74.5041627751 meter * newton but the right hand side evaluated to 74.5040725471 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00012%) Warning: Constraint [-B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)*G_BladeElement... >= dT_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,) [lbf]...] is not tight because the left hand side evaluated to 134.449579759 kilogram * meter / second ** 2 but the right hand side evaluated to 30.2255018449 force_pound (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(0,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.420585903433 meter ** 2 / second ** 2 but the right hand side evaluated to 0.42057303321 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0031%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(1,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.314644998908 meter ** 2 / second ** 2 but the right hand side evaluated to 0.314629685653 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0049%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(2,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.16893640237 meter ** 2 / second ** 2 but the right hand side evaluated to 0.168931506563 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0029%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(3,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.063964051843 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0639630073546 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0016%) Warning: Constraint [0.151*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**-2*F_Bla... >= 0.00633*B_BladeElement_Propulsor_Test/PropulsorPerf.2/BladeElementProp/BladeElementPerf_(4,)**2*G_Bl...] is not tight because the left hand side evaluated to 0.0226356673111 meter ** 2 / second ** 2 but the right hand side evaluated to 0.0226353930664 meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.0012%) Using solver 'mosek' Solving for 13 variables. Solving took 0.034 seconds. Beginning signomial solve. Solving took 11 GP solves and 1.99 seconds. Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619897.4143 but bound is 700000.0000 Using solver 'mosek_cli' Solving for 13 variables. Solving took 0.181 seconds. Beginning signomial solve. Solving took 11 GP solves and 3.52 seconds. Warning: Constraint [omega_BladeElementProp/BladeElementPerf_(0,)*r_BladeElementProp/BladeElementPerf_(0,) [m*rpm]... >= Wt_BladeElementProp/BladeElementPerf_(0,) + vt_BladeElementProp/BladeElementPerf_(0,) [m/s]...] is not tight because the left hand side evaluated to 147.268875342 meter * revolutions_per_minute but the right hand side evaluated to 15.4219435408 meter / second (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Constraint [dQ_BladeElementProp/BladeElementPerf_(3,) [N*m]... >= B_BladeElementProp/BladeElementPerf_(3,)*G_BladeElementProp/BladeElementPerf_(3,)*Wa_BladeElementPro...] is not tight because the left hand side evaluated to 42.7884411703 meter * newton but the right hand side evaluated to 42.7884887635 kilogram * meter ** 2 / second ** 2 (Allowable error: 0.0001%, Actual error: 0.00011%) Warning: Variable [cl_BladeElementProp/BladeElementPerf_(0,), cl_BladeElementProp/BladeElementPerf_(1,), cl_BladeEleme could cause inaccurate result because it is below lower bound. Solution is 0.6000 but bound is 0.4742 Warning: Variable [Re_BladeElementProp/BladeElementPerf_(0,), Re_BladeElementProp/BladeElementPerf_(1,), Re_BladeEleme could cause inaccurate result because it is above upper bound. Solution is 1619891.9379 but bound is 700000.0000 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 2223878.3883 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 1853897.0659 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853897.0663 but bound is 1000000.0000 Warning: Variable Re_TailAero could cause inaccurate result because it is above upper bound. Solution is 2220959.7939 but bound is 1000000.0000 Warning: Variable Re_TailAero.1 could cause inaccurate result because it is above upper bound. Solution is 2499796.7837 but bound is 1000000.0000 Warning: Variable Re_TailAero.2 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.3 could cause inaccurate result because it is above upper bound. Solution is 1860712.4314 but bound is 1000000.0000 Warning: Variable Re_TailAero.4 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_TailAero.5 could cause inaccurate result because it is above upper bound. Solution is 1853896.1324 but bound is 1000000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1884891.2729 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1910419.4978 but bound is 700000.0000 Warning: Variable Re_WingAero could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000 Warning: Variable Re_WingAero.1 could cause inaccurate result because it is above upper bound. Solution is 1910412.9866 but bound is 700000.0000 Running tests... ---------------------------------------------------------------------- .......... ---------------------------------------------------------------------- Ran 10 tests in 20.054s OK Generating XML reports... Cloning into 'eVTOL'... 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Finally, we hope you find our documentation (https://gpkit.readthedocs.io/) and engineering-design models (https://github.com/convexengineering/gplibrary/) to be useful resources for your own applications. Enjoy! USING LOCAL DIRECTORY AS GPKITMODELS DIRECTORY calling ['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(<type 'str'>, {}) calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gassolar.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/jho.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['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(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'gpkit-models branch': 'master'}) calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/SPaircraft.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'skipsolvers': 'cvxopt, mosek_cli', 'pip install': 'git+https://github.com/hoburg/turbofan.git', 'gpkit-models branch': 'master'}) calling ['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(<type 'str'>, {'skipsolvers': 'cvxopt', 'pip install': 'pandas, git+https://github.com/convexengineering/gpfit.git, git+https://github.com/convexengineering/gassolar.git', 'gpkit-models branch': 'master'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gpfit.git'] attempt 1 calling ['pip', 'install', 'git+https://github.com/convexengineering/gassolar.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/gplibrary.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {'pip install': 'pandas, git+https://github.com/hoburg/gpfit.git'}) calling ['pip', 'install', 'pandas'] attempt 1 calling ['pip', 'install', 'git+https://github.com/hoburg/gpfit.git'] attempt 1 calling ['pip', 'install', '.'] attempt 1 calling ['git', 'clone', '--depth', '1', '-b', 'master', 'https://github.com/convexengineering/eVTOL.git'] attempt 1 SETTINGS defaultdict(<type 'str'>, {}) ---------------------------------------------------------------------- Ran 233 tests in 52.082s OK (venv2_gpkit) (base) D:\jenkins\workspace\gplibrary_PR_Models\mosek>exit 0 [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 'D:\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