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gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171115181111)

Failing for the past 1 build (Since Failed #22 )
Took 3.4 sec.

Error Message

'V_v'

Stacktrace

Traceback (most recent call last):
  File "c:\users\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "c:\users\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "c:\users\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 41, in test_fn
    mod.test()
  File "jho.py", line 356, in test
  File "c:\users\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows10x64\optimizer\mosek\gpkit\gpkit\keydict.py", line 153, in __setitem__
    key, idx = self.parse_and_index(key)
  File "c:\users\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows10x64\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 -7.60691943463e-12.
Allowing negative dual variable(s) as small as -6.61484755859e-14.
Allowing negative dual variable(s) as small as -5.41762815165e-13.
Allowing negative dual variable(s) as small as -5.41314389146e-13.
Allowing negative dual variable(s) as small as -4.02640811317e-13.
Allowing negative dual variable(s) as small as -9.68948228944e-13.
Allowing negative dual variable(s) as small as -1.27195975107e-12.
Allowing negative dual variable(s) as small as -1.27457029306e-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 -1.21137236526e-12.
Allowing negative dual variable(s) as small as -1.3062493795e-12.
Allowing negative dual variable(s) as small as -1.6997288993e-12.
Allowing negative dual variable(s) as small as -1.70081440251e-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 -2.31796416149e-11.
Allowing negative dual variable(s) as small as -3.03673609568e-12.
Allowing negative dual variable(s) as small as -2.85201994172e-12.
Allowing negative dual variable(s) as small as -2.81110472058e-12.
Solving took 4 GP solves and 6.17 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.09577710689e-12.
Allowing negative dual variable(s) as small as -2.20925014394e-12.
Allowing negative dual variable(s) as small as -2.2090333035e-12.
Solving took 4 GP solves and 2.05 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -7.60672254352e-12.
Allowing negative dual variable(s) as small as -6.61545471181e-14.
Allowing negative dual variable(s) as small as -5.41829602019e-13.
Allowing negative dual variable(s) as small as -5.4152082124e-13.
Allowing negative dual variable(s) as small as -4.06326665023e-13.
Allowing negative dual variable(s) as small as -9.70054765681e-13.
Allowing negative dual variable(s) as small as -1.27245046097e-12.
Allowing negative dual variable(s) as small as -1.27393928739e-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 -1.21198212057e-12.
Allowing negative dual variable(s) as small as -1.30721692151e-12.
Allowing negative dual variable(s) as small as -1.70121859308e-12.
Allowing negative dual variable(s) as small as -1.70154493793e-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 -2.31796801165e-11.
Allowing negative dual variable(s) as small as -3.03674587538e-12.
Allowing negative dual variable(s) as small as -2.85195640621e-12.
Allowing negative dual variable(s) as small as -2.81097696747e-12.
Solving took 4 GP solves and 10.6 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.09615527661e-12.
Allowing negative dual variable(s) as small as -2.20769930115e-12.
Allowing negative dual variable(s) as small as -2.20495323389e-12.
Solving took 4 GP solves and 2.25 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error