Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210816154751)
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 0.47 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.298 seconds. Solved cost was 4.003e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7517 chars]... 97.19565801947527] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46201752005214] dimensionless Wing Cd percent Diff: [-29.7021153] Induced Drag Cd Percent Diff: [-33.70519935] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63167736] FUSELAGE DIFFERENCES Weight of HB material: -48.55958173859139 Weight of VB material: 117.25632853170637 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.802691]
Standard Error
/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys/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]))