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
NameError: global name 'M' is not defined

Standard Output

Allowing negative dual variable(s) as small as -1.21198190373e-13.
Allowing negative dual variable(s) as small as -8.14348588563e-14.
Allowing negative dual variable(s) as small as -2.07863240509e-14.
Allowing negative dual variable(s) as small as -2.06709649397e-14.
Allowing negative dual variable(s) as small as -1.04084254236e-12.
Allowing negative dual variable(s) as small as -1.64693367451e-12.
Allowing negative dual variable(s) as small as -1.46349490686e-12.
Allowing negative dual variable(s) as small as -1.4643655212e-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 -1.12020722559e-12.
Allowing negative dual variable(s) as small as -1.65538719885e-12.
Allowing negative dual variable(s) as small as -1.63856948843e-12.
Allowing negative dual variable(s) as small as -1.63844241993e-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 -1.25445656776e-11.
Allowing negative dual variable(s) as small as -4.86405584922e-11.
Allowing negative dual variable(s) as small as -4.13816859489e-12.
Allowing negative dual variable(s) as small as -4.13935402382e-12.
Solving took 4 GP solves and 3.52 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.13 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21185179947e-13.
Allowing negative dual variable(s) as small as -8.15458811587e-14.
Allowing negative dual variable(s) as small as -2.07438233257e-14.
Allowing negative dual variable(s) as small as -2.07698441779e-14.
Allowing negative dual variable(s) as small as -1.04775042808e-12.
Allowing negative dual variable(s) as small as -1.64772145581e-12.
Allowing negative dual variable(s) as small as -1.46369765266e-12.
Allowing negative dual variable(s) as small as -1.46878321138e-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 -1.1214594791e-12.
Allowing negative dual variable(s) as small as -1.65718610709e-12.
Allowing negative dual variable(s) as small as -1.63720751366e-12.
Allowing negative dual variable(s) as small as -1.63925318632e-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 -1.25444171048e-11.
Allowing negative dual variable(s) as small as -4.86406774991e-11.
Allowing negative dual variable(s) as small as -4.13813603127e-12.
Allowing negative dual variable(s) as small as -4.13942781682e-12.
Solving took 4 GP solves and 3.07 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.86 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364

Failed

Error Message

Stacktrace

Standard Output

Standard Error