Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20210816211427)
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 0.701 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4699 posynomial inequalities. Solving took 0.515 seconds. Solved cost was 3.998e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 7471 chars]... t Diff: [-97.19567274] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.4743193] dimensionless Wing Cd percent Diff: [-29.70476338] Induced Drag Cd Percent Diff: [-33.71067922] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63110448] FUSELAGE DIFFERENCES Weight of HB material: -48.57617054527538 Weight of VB material: 117.29547614961275 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.8025859]
Standard Error
/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:431: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])