Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200718011050)

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 0.46 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.369 seconds.
Solved cost was 4.006e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 8469 chars]...
9562613672196] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.468989880822136] dimensionless


Wing Cd percent Diff: [-29.70360281]
Induced Drag Cd Percent Diff: [-33.70824252]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63108165]




FUSELAGE DIFFERENCES




Weight of HB material: -48.56205100393667 


Weight of VB material: 117.3163805653055 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80262719]
	

Standard Error

/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys_VM/optimizer/mosek/gpkit/constraints/gp.py:407: RuntimeWarning: divide by zero encountered in log
  for i, mi in enumerate(self.m_idxs) if la[i])