Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180110083840)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.652383521151158e-13.
Allowing negative dual variable(s) as small as -4.4698858329972335e-13.
Allowing negative dual variable(s) as small as -7.988271502612498e-14.
Allowing negative dual variable(s) as small as -9.648206712731255e-14.
Solving took 4 GP solves and 4.9 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.6471836875319177e-13.
Allowing negative dual variable(s) as small as -4.715151880052559e-13.
Allowing negative dual variable(s) as small as -1.030976519433846e-13.
Allowing negative dual variable(s) as small as -7.552660753751272e-14.
Solving took 4 GP solves and 169 seconds.
MTOW [lbs] = 132.52
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 = 20.351
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] = 27.299
optimum loiter speed for min power, start of loiter [m/s] = 23.617
optimum loiter speed for min power, end of loiter [m/s] = 16.684
optimum cruise speed, inbound [m/s] = 31.019
optimum cruise speed, outbound [m/s] = 23.408
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.027305037962856e-12.
Allowing negative dual variable(s) as small as -1.1071728783066873e-12.
Allowing negative dual variable(s) as small as -2.483316467476059e-12.
Allowing negative dual variable(s) as small as -2.4819337837556194e-12.
Solving took 4 GP solves and 50.2 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.82 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
MTOW [lbs] = 132.52
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 = 20.351
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] = 27.299
optimum loiter speed for min power, start of loiter [m/s] = 23.617
optimum loiter speed for min power, end of loiter [m/s] = 16.684
optimum cruise speed, inbound [m/s] = 31.019
optimum cruise speed, outbound [m/s] = 23.408
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.027275898772156e-12.
Allowing negative dual variable(s) as small as -1.1070943224826167e-12.
Allowing negative dual variable(s) as small as -2.483370274011534e-12.
Allowing negative dual variable(s) as small as -2.481984975278702e-12.
Solving took 4 GP solves and 4.27 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 14.6 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
	

Standard Error