Failed
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
)
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