Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200714174802)
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 0.631 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.513 seconds. Solved cost was 4.014e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 8428 chars]... Diff: [-97.1956568] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46425659] dimensionless Wing Cd percent Diff: [-29.70294072] Induced Drag Cd Percent Diff: [-33.70722013] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63170951] FUSELAGE DIFFERENCES Weight of HB material: -48.56200619584277 Weight of VB material: 117.27406998061402 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80266544]
Standard Error
/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:407: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])