Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20210321174517)
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 0.573 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.263 seconds. Solved cost was 4.009e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7517 chars]... 9565713216207] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46169689114646] dimensionless Wing Cd percent Diff: [-29.70224932] Induced Drag Cd Percent Diff: [-33.70550596] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63192738] FUSELAGE DIFFERENCES Weight of HB material: -48.55856004255536 Weight of VB material: 117.25688627775398 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80269231]
Standard Error
/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:426: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])