Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20220329204800)
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_conif' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.183 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_conif' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.171 seconds. Solved cost was 2.96e+10. GP Solve 3 Using solver 'mosek_co ...[truncated 1894 chars]... .19562346854258] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.45988427002766] dimensionless Wing Cd percent Diff: [-29.70195523] Induced Drag Cd Percent Diff: [-33.70462132] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.6322152] FUSELAGE DIFFERENCES Weight of HB material: -48.55968142917282 Weight of VB material: 117.26903108617512 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80271009]
Standard Error
/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:441: RuntimeWarning: divide by zero encountered in log b[mi] - np.log(self.nu_by_posy[i]/la[i]))