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gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115182157)

Failing for the past 1 build (Since Failed #22 )
Took 2.3 sec.

Error Message

'V_v'

Stacktrace

Traceback (most recent call last):
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 41, in test_fn
    mod.test()
  File "jho.py", line 356, in test
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\keydict.py", line 153, in __setitem__
    key, idx = self.parse_and_index(key)
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\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 -1.21258038333e-13.
Allowing negative dual variable(s) as small as -8.14365935797e-14.
Allowing negative dual variable(s) as small as -2.07299455379e-14.
Allowing negative dual variable(s) as small as -2.05131051034e-14.
Allowing negative dual variable(s) as small as -1.04257379639e-12.
Allowing negative dual variable(s) as small as -1.64371879822e-12.
Allowing negative dual variable(s) as small as -1.46173958354e-12.
Allowing negative dual variable(s) as small as -1.45930403178e-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 -1.12587413351e-12.
Allowing negative dual variable(s) as small as -1.66058529774e-12.
Allowing negative dual variable(s) as small as -1.63371898475e-12.
Allowing negative dual variable(s) as small as -1.64062665363e-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 -1.25444302825e-11.
Allowing negative dual variable(s) as small as -4.86404706343e-11.
Allowing negative dual variable(s) as small as -4.13824961427e-12.
Allowing negative dual variable(s) as small as -4.13945348869e-12.
Solving took 4 GP solves and 35.9 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 6.56 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21093239602e-13.
Allowing negative dual variable(s) as small as -8.13186323834e-14.
Allowing negative dual variable(s) as small as -2.06449440876e-14.
Allowing negative dual variable(s) as small as -2.06527503432e-14.
Allowing negative dual variable(s) as small as -1.0381383253e-12.
Allowing negative dual variable(s) as small as -1.64983695108e-12.
Allowing negative dual variable(s) as small as -1.46531593283e-12.
Allowing negative dual variable(s) as small as -1.46755979764e-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 -1.1277467675e-12.
Allowing negative dual variable(s) as small as -1.6578999458e-12.
Allowing negative dual variable(s) as small as -1.63619118254e-12.
Allowing negative dual variable(s) as small as -1.63735865144e-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 -1.25445155165e-11.
Allowing negative dual variable(s) as small as -4.86405175029e-11.
Allowing negative dual variable(s) as small as -4.13812243341e-12.
Allowing negative dual variable(s) as small as -4.13932788614e-12.
Solving took 4 GP solves and 31.9 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 4.66 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364

Standard Error