Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200416162330)
Standard Output
Starting a sequence of GP solves for 317 free variables in 136 locally-GP constraints and for 1198 free variables in 4705 posynomial inequalities. GP Solve 1 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.387 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.331 seconds. Solved cost was 4.01e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 8469 chars]... 1957682702787] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46689856667439] dimensionless Wing Cd percent Diff: [-29.70338958] Induced Drag Cd Percent Diff: [-33.70895417] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63120633] FUSELAGE DIFFERENCES Weight of HB material: -48.56411390849966 Weight of VB material: 117.22048168813754 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80264357]
Standard Error
/Users/jenkins/workspace/CE_RM_SPaircraft_Push/mosek/gpkit/gpkit/constraints/gp.py:403: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])