Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210319171452)
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 44.4 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.719 seconds. Solved cost was 4.012e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7456 chars]... Diff: [-97.19571798] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.48030973] dimensionless Wing Cd percent Diff: [-29.70585871] Induced Drag Cd Percent Diff: [-33.71263253] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63100651] FUSELAGE DIFFERENCES Weight of HB material: -48.58502818861035 Weight of VB material: 117.27130623043598 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80255444]
Standard Error
/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/reynolds/optimizer/mosek/gpkit/constraints/gp.py:426: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])