Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180111113842)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.8665589867082897e-13.
Allowing negative dual variable(s) as small as -5.070882949653743e-13.
Allowing negative dual variable(s) as small as -1.1294025610564251e-13.
Allowing negative dual variable(s) as small as -1.170476476158866e-13.
Solving took 4 GP solves and 2.75 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.0070303885798566e-13.
Allowing negative dual variable(s) as small as -5.126912349523449e-13.
Allowing negative dual variable(s) as small as -9.81237660568901e-14.
Allowing negative dual variable(s) as small as -1.1988392049910868e-13.
Solving took 4 GP solves and 2.75 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 -5.027353962519715e-12.
Allowing negative dual variable(s) as small as -1.1070982176810843e-12.
Allowing negative dual variable(s) as small as -2.483316863685646e-12.
Allowing negative dual variable(s) as small as -2.4820605596863782e-12.
Solving took 4 GP solves and 2.43 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.25 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 -5.027316089439947e-12.
Allowing negative dual variable(s) as small as -1.107254737297863e-12.
Allowing negative dual variable(s) as small as -2.483296450163493e-12.
Allowing negative dual variable(s) as small as -2.4820923255676068e-12.
Solving took 4 GP solves and 2.71 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.85 seconds.
Max payload weight [lbf] = 9.202
Max take off weight [lbf] = 140.328
	

Standard Error