Traceback (most recent call last):
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\helpers.py", line 62, in test
    testfn(name, import_dict, path)(self)
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\optimizer\mosek\gpkit\gpkit\tests\from_paths.py", line 50, in <lambda>
    lambda self: getattr(self, name)()))  # pylint:disable=undefined-variable
  File "d:\jenkins\workspace\gpkit_researchmodel_jho_pr\buildnode\windows7x64\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 -1.21116658369e-13.
Allowing negative dual variable(s) as small as -8.15562894996e-14.
Allowing negative dual variable(s) as small as -2.07681094544e-14.
Allowing negative dual variable(s) as small as -2.06787711954e-14.
Allowing negative dual variable(s) as small as -1.04394444478e-12.
Allowing negative dual variable(s) as small as -1.6523199909e-12.
Allowing negative dual variable(s) as small as -1.46156437647e-12.
Allowing negative dual variable(s) as small as -1.46453964407e-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 -1.12470623093e-12.
Allowing negative dual variable(s) as small as -1.6567528599e-12.
Allowing negative dual variable(s) as small as -1.64171042212e-12.
Allowing negative dual variable(s) as small as -1.63591644571e-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 -1.25444897575e-11.
Allowing negative dual variable(s) as small as -4.86405767805e-11.
Allowing negative dual variable(s) as small as -4.13816686217e-12.
Allowing negative dual variable(s) as small as -4.13942155031e-12.
Solving took 4 GP solves and 15.5 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 15.8 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21300539058e-13.
Allowing negative dual variable(s) as small as -8.14912373692e-14.
Allowing negative dual variable(s) as small as -2.06596892371e-14.
Allowing negative dual variable(s) as small as -2.05885655746e-14.
Allowing negative dual variable(s) as small as -1.04105634703e-12.
Allowing negative dual variable(s) as small as -1.65249021064e-12.
Allowing negative dual variable(s) as small as -1.46166455675e-12.
Allowing negative dual variable(s) as small as -1.46543909819e-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 -1.12642512505e-12.
Allowing negative dual variable(s) as small as -1.65428911889e-12.
Allowing negative dual variable(s) as small as -1.6334162755e-12.
Allowing negative dual variable(s) as small as -1.63950775699e-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 -1.25445300179e-11.
Allowing negative dual variable(s) as small as -4.8640657348e-11.
Allowing negative dual variable(s) as small as -4.1382402902e-12.
Allowing negative dual variable(s) as small as -4.13928922846e-12.
Solving took 4 GP solves and 11.5 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 19.5 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364

Failed

Error Message

Stacktrace

Standard Output

Standard Error