Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20210310182922)
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 0.579 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.558 seconds. Solved cost was 4.008e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7472 chars]... iff: [-97.19580752] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.47089544] dimensionless Wing Cd percent Diff: [-29.70426281] Induced Drag Cd Percent Diff: [-33.71080805] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63088976] FUSELAGE DIFFERENCES Weight of HB material: -48.566237340559624 Weight of VB material: 117.21038134647485 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80260851]
Standard Error
/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/reynolds/optimizer/mosek/gpkit/constraints/gp.py:398: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])