Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200714221716)
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 0.648 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.266 seconds. Solved cost was 4.015e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 8465 chars]... 97.19567815599765] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.4728922840732] dimensionless Wing Cd percent Diff: [-29.7041974] Induced Drag Cd Percent Diff: [-33.7098455] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63026856] FUSELAGE DIFFERENCES Weight of HB material: -48.5665547351064 Weight of VB material: 117.30029681722526 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80259272]
Standard Error
/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys_VM/optimizer/mosek/gpkit/constraints/gp.py:407: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])