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gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171115180901)

Failing for the past 1 build (Since Failed #22 )
Took 3.3 sec.

Error Message

'V_v'

Stacktrace

Traceback (most recent call last):
  File "/Users/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "/Users/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "/Users/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/macys/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 41, in test_fn
    mod.test()
  File "jho.py", line 356, in test
  File "/Users/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/macys/optimizer/mosek/gpkit/gpkit/keydict.py", line 153, in __setitem__
    key, idx = self.parse_and_index(key)
  File "/Users/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/macys/optimizer/mosek/gpkit/gpkit/keydict.py", line 104, in parse_and_index
    raise KeyError(key)
KeyError: 'V_v'

Standard Output

Allowing negative dual variable(s) as small as -1.21175638967e-13.
Allowing negative dual variable(s) as small as -8.15918513308e-14.
Allowing negative dual variable(s) as small as -2.06232600442e-14.
Allowing negative dual variable(s) as small as -2.06831080041e-14.
Allowing negative dual variable(s) as small as -1.04669007836e-12.
Allowing negative dual variable(s) as small as -1.64441095289e-12.
Allowing negative dual variable(s) as small as -1.46568672997e-12.
Allowing negative dual variable(s) as small as -1.46422349072e-12.
MTOW [lbs] = 132.53
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.1216975699e-12.
Allowing negative dual variable(s) as small as -1.6573582784e-12.
Allowing negative dual variable(s) as small as -1.63922868335e-12.
Allowing negative dual variable(s) as small as -1.63803606096e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25444586304e-11.
Allowing negative dual variable(s) as small as -4.86404146735e-11.
Allowing negative dual variable(s) as small as -4.13825648708e-12.
Allowing negative dual variable(s) as small as -4.13939883336e-12.
Solving took 4 GP solves and 14.4 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 8.74 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21199057734e-13.
Allowing negative dual variable(s) as small as -8.14504713675e-14.
Allowing negative dual variable(s) as small as -2.07689768161e-14.
Allowing negative dual variable(s) as small as -2.07256087292e-14.
Allowing negative dual variable(s) as small as -1.04410143725e-12.
Allowing negative dual variable(s) as small as -1.64585966383e-12.
Allowing negative dual variable(s) as small as -1.46543476139e-12.
Allowing negative dual variable(s) as small as -1.46640837494e-12.
MTOW [lbs] = 132.53
Zero fuel weight [lbs] = 53.63
Wing span [ft] = 24.00
Aicraft length [ft] = 12.90
Aspect ratio = 25.60
mean aerodynamic chord [ft] = 0.9722
root chord [ft] = 1.250
speed for best rate of climb [m/s]: Vy = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12376124031e-12.
Allowing negative dual variable(s) as small as -1.65560143719e-12.
Allowing negative dual variable(s) as small as -1.641330084e-12.
Allowing negative dual variable(s) as small as -1.63712381325e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25445087236e-11.
Allowing negative dual variable(s) as small as -4.86405516669e-11.
Allowing negative dual variable(s) as small as -4.13814352697e-12.
Allowing negative dual variable(s) as small as -4.13934303446e-12.
Solving took 4 GP solves and 15.3 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 7.88 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364

Standard Error