Passed

gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20220302153917)

Standard Output

Starting a sequence of GP solves
 for 317 free variables
  in 136 locally-GP constraints
  and for 1198 free variables
       in 4699 posynomial inequalities.

GP Solve 1
Using solver 'mosek_conif'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.359 seconds.
Solved cost was 3.965e+40.

GP Solve 2
Using solver 'mosek_conif'
 for 1198 free variables
  in 4699 posynomial inequalities.
Solving took 0.326 seconds.
Solved cost was 2.96e+10.

GP Solve 3
Using solver 'mosek_co
...[truncated 1891 chars]...
.19562346854258] dimensionless


Fuselage Cd Percent Diff: [108.78752887]


VT Cd Percent Diff: [-35.45988427002766] dimensionless


Wing Cd percent Diff: [-29.70195523]
Induced Drag Cd Percent Diff: [-33.70462132]




CRUISE SEGMENT 1 TSFC DIFFERENCES


Initial Cruise TSFC Percent Diff: [-5.6322152]




FUSELAGE DIFFERENCES




Weight of HB material: -48.55968142917282 


Weight of VB material: 117.26903108617512 
Fan Propulsive Efficiency in Cruise Segment 1
---------------------
[0.80271009]

Standard Error

/Users/jenkins/workspace/CE_gpkit_PR_research_models/buildnode/macys/optimizer/mosek/gpkit/constraints/gp.py:441: RuntimeWarning: divide by zero encountered in log
  b[mi] - np.log(self.nu_by_posy[i]/la[i]))