Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200715175715)

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 0.492 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.256 seconds.
Solved cost was 4.013e+10.

GP Solve 3
Using solver 'mosek_cli'
...[truncated 8478 chars]...
583679064598] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.47397086807222] dimensionless


Wing Cd percent Diff: [-29.70468816]
Induced Drag Cd Percent Diff: [-33.71169093]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63041854]




FUSELAGE DIFFERENCES




Weight of HB material: -48.573984132691876 


Weight of VB material: 117.20694298269244 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80258349]
	

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])