Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20210714225908)
Standard Output
Starting a sequence of GP solves for 317 free variables in 136 locally-GP constraints and for 1198 free variables in 4699 posynomial inequalities. GP Solve 1 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.957 seconds. Solved cost was 3.964e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 1.03 seconds. Solved cost was 4.016e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7509 chars]... 19566185995136] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46197618520338] dimensionless Wing Cd percent Diff: [-29.70221581] Induced Drag Cd Percent Diff: [-33.7054874] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63173278] FUSELAGE DIFFERENCES Weight of HB material: -48.55910337835982 Weight of VB material: 117.25595705573251 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80269078]
Standard Error
/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys_VM/optimizer/mosek/gpkit/constraints/gp.py:437: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])