Failed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171115182640)
Failing for the past 1 build
(Since Failed
)
Error Message
global name 'M' is not defined
Stacktrace
Traceback (most recent call last): File "/Users/jenkins/workspace/gpkit_ResearchModel_jho_PR/buildnode/macys_Sierra/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_Sierra/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_Sierra/optimizer/mosek/gpkit/gpkit/tests/from_paths.py", line 41, in test_fn mod.test() File "jho.py", line 356, in test NameError: global name 'M' is not defined
Standard Output
Allowing negative dual variable(s) as small as -7.60690989365e-12. Allowing negative dual variable(s) as small as -6.60600046887e-14. Allowing negative dual variable(s) as small as -5.41837408274e-13. Allowing negative dual variable(s) as small as -5.41937154874e-13. Allowing negative dual variable(s) as small as -4.03237122512e-13. Allowing negative dual variable(s) as small as -9.67772736948e-13. Allowing negative dual variable(s) as small as -1.274263247e-12. Allowing negative dual variable(s) as small as -1.27194131963e-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 -1.20987074526e-12. Allowing negative dual variable(s) as small as -1.30606918509e-12. Allowing negative dual variable(s) as small as -1.70088661038e-12. Allowing negative dual variable(s) as small as -1.70274514974e-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 -2.31796546225e-11. Allowing negative dual variable(s) as small as -3.03674388444e-12. Allowing negative dual variable(s) as small as -2.8520668459e-12. Allowing negative dual variable(s) as small as -2.81106155973e-12. Solving took 4 GP solves and 3.05 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.09638946427e-12. Allowing negative dual variable(s) as small as -2.20758654412e-12. Allowing negative dual variable(s) as small as -2.20392974704e-12. Solving took 4 GP solves and 2.65 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -7.60690989365e-12. Allowing negative dual variable(s) as small as -6.60600046887e-14. Allowing negative dual variable(s) as small as -5.41837408274e-13. Allowing negative dual variable(s) as small as -5.41937154874e-13. Allowing negative dual variable(s) as small as -4.03237122512e-13. Allowing negative dual variable(s) as small as -9.67772736948e-13. Allowing negative dual variable(s) as small as -1.274263247e-12. Allowing negative dual variable(s) as small as -1.27194131963e-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 -1.20987074526e-12. Allowing negative dual variable(s) as small as -1.30606918509e-12. Allowing negative dual variable(s) as small as -1.70088661038e-12. Allowing negative dual variable(s) as small as -1.70274514974e-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 -2.31796546225e-11. Allowing negative dual variable(s) as small as -3.03674388444e-12. Allowing negative dual variable(s) as small as -2.8520668459e-12. Allowing negative dual variable(s) as small as -2.81106155973e-12. Solving took 4 GP solves and 3.1 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.09638946427e-12. Allowing negative dual variable(s) as small as -2.20758654412e-12. Allowing negative dual variable(s) as small as -2.20392974704e-12. Solving took 4 GP solves and 2.57 seconds. Max payload weight [lbf] = 8.892 Max take off weight [lbf] = 140.364