Failed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115180956)
Failing for the past 1 build
(Since Failed
)
Error Message
'V_v'
Stacktrace
Traceback (most recent call last): File "/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/tests/helpers.py", line 62, in test testfn(name, import_dict, path)(self) File "/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 50, in <lambda> lambda self: getattr(self, name)())) # pylint:disable=undefined-variable File "/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 41, in test_fn mod.test() File "jho.py", line 356, in test File "/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/reynolds/optimizer/mosek/gpkit/gpkit/keydict.py", line 153, in __setitem__ key, idx = self.parse_and_index(key) File "/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/reynolds/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 -1.21134872966e-13. Allowing negative dual variable(s) as small as -8.1382817152e-14. Allowing negative dual variable(s) as small as -2.07221392823e-14. Allowing negative dual variable(s) as small as -2.05686162547e-14. Allowing negative dual variable(s) as small as -1.04649470513e-12. Allowing negative dual variable(s) as small as -1.6471277467e-12. Allowing negative dual variable(s) as small as -1.46450690117e-12. Allowing negative dual variable(s) as small as -1.46574419269e-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 -1.13169716653e-12. Allowing negative dual variable(s) as small as -1.65434419636e-12. Allowing negative dual variable(s) as small as -1.63504366296e-12. Allowing negative dual variable(s) as small as -1.64076803359e-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 -1.25445698033e-11. Allowing negative dual variable(s) as small as -4.86405968411e-11. Allowing negative dual variable(s) as small as -4.13818927991e-12. Allowing negative dual variable(s) as small as -4.13941169686e-12. Solving took 4 GP solves and 2.96 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.82 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -1.21114923646e-13. Allowing negative dual variable(s) as small as -8.14582776232e-14. Allowing negative dual variable(s) as small as -2.06206579589e-14. Allowing negative dual variable(s) as small as -2.07516295814e-14. Allowing negative dual variable(s) as small as -1.03920843285e-12. Allowing negative dual variable(s) as small as -1.64634126644e-12. Allowing negative dual variable(s) as small as -1.46239921214e-12. Allowing negative dual variable(s) as small as -1.46779637056e-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 -1.1271981612e-12. Allowing negative dual variable(s) as small as -1.65860142461e-12. Allowing negative dual variable(s) as small as -1.63594094868e-12. Allowing negative dual variable(s) as small as -1.6389248899e-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 -1.25444629358e-11. Allowing negative dual variable(s) as small as -4.86406004485e-11. Allowing negative dual variable(s) as small as -4.13814078108e-12. Allowing negative dual variable(s) as small as -4.13940376258e-12. Solving took 4 GP solves and 2.64 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.68 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364