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

Failed

Error Message

Stacktrace

Standard Output

Standard Error