Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20210816155133)
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 0.486 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.289 seconds. Solved cost was 4.014e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7509 chars]... .1956471580275] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46114685232066] dimensionless Wing Cd percent Diff: [-29.70240044] Induced Drag Cd Percent Diff: [-33.70573158] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63242179] FUSELAGE DIFFERENCES Weight of HB material: -48.55800917720656 Weight of VB material: 117.25904197837012 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80269555]
Standard Error
/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys_VM/optimizer/mosek/gpkit/constraints/gp.py:430: RuntimeWarning: divide by zero encountered in log b[mi] - np.log(self.nu_by_posy[i]/la[i]))