Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20201118151500)
Standard Output
Starting a sequence of GP solves for 317 free variables in 136 locally-GP constraints and for 1198 free variables in 4705 posynomial inequalities. GP Solve 1 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.343 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.275 seconds. Solved cost was 4.02e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 8467 chars]... 19565921761395] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46192787311985] dimensionless Wing Cd percent Diff: [-29.70222386] Induced Drag Cd Percent Diff: [-33.70547895] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63186376] FUSELAGE DIFFERENCES Weight of HB material: -48.56037347011905 Weight of VB material: 117.2560035370157 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80269216]
Standard Error
/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys_VM/optimizer/mosek/gpkit/constraints/gp.py:431: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])