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
NameError: global name 'M' is not defined

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 -4.03949443339e-13.
Allowing negative dual variable(s) as small as -9.72400979182e-13.
Allowing negative dual variable(s) as small as -1.27212823609e-12.
Allowing negative dual variable(s) as small as -1.27474636749e-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 -1.2132066185e-12.
Allowing negative dual variable(s) as small as -1.30722776354e-12.
Allowing negative dual variable(s) as small as -1.70129665564e-12.
Allowing negative dual variable(s) as small as -1.69964758413e-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 -2.31795207741e-11.
Allowing negative dual variable(s) as small as -3.36300555508e-12.
Allowing negative dual variable(s) as small as -2.85199159793e-12.
Allowing negative dual variable(s) as small as -2.81109609361e-12.
Solving took 4 GP solves and 18.1 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.09972880697e-12.
Allowing negative dual variable(s) as small as -2.21547086232e-12.
Allowing negative dual variable(s) as small as -2.21625322261e-12.
Solving took 4 GP solves and 17.6 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -7.60652651977e-12.
Allowing negative dual variable(s) as small as -6.60070956227e-14.
Allowing negative dual variable(s) as small as -5.41901593043e-13.
Allowing negative dual variable(s) as small as -5.41365563489e-13.
Allowing negative dual variable(s) as small as -4.01413060777e-13.
Allowing negative dual variable(s) as small as -9.69554081118e-13.
Allowing negative dual variable(s) as small as -1.27265992883e-12.
Allowing negative dual variable(s) as small as -1.27237044685e-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 -1.21306957535e-12.
Allowing negative dual variable(s) as small as -1.3070098389e-12.
Allowing negative dual variable(s) as small as -1.69848575308e-12.
Allowing negative dual variable(s) as small as -1.6984252546e-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 -2.3179649303e-11.
Allowing negative dual variable(s) as small as -3.03680031429e-12.
Allowing negative dual variable(s) as small as -2.85198644993e-12.
Allowing negative dual variable(s) as small as -2.81114454098e-12.
Solving took 4 GP solves and 2.39 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.0989186911e-12.
Allowing negative dual variable(s) as small as -2.20766113723e-12.
Allowing negative dual variable(s) as small as -2.2053608939e-12.
Solving took 4 GP solves and 2.54 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364

Failed

Error Message

Stacktrace

Standard Output

Standard Error