Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200807225353)
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 0.356 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.299 seconds. Solved cost was 4.016e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 8457 chars]... 19577389689856] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.46839178360587] dimensionless Wing Cd percent Diff: [-29.70399059] Induced Drag Cd Percent Diff: [-33.70999091] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.6316365] FUSELAGE DIFFERENCES Weight of HB material: -48.56827568740606 Weight of VB material: 117.21382419620241 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80263159]
Standard Error
/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:407: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])