Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200715061911)

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 0.306 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_cli'
 for 1198 free variables
  in 4705 posynomial inequalities.
Solving took 0.26 seconds.
Solved cost was 4.009e+10.

GP Solve 3
Using solver 'mosek_cli'

...[truncated 8466 chars]...
9585682962033] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.47524300932485] dimensionless


Wing Cd percent Diff: [-29.70499848]
Induced Drag Cd Percent Diff: [-33.71254764]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.63063796]




FUSELAGE DIFFERENCES




Weight of HB material: -48.57964106717352 


Weight of VB material: 117.19786145169972 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80257716]
	

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])