Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428101949)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.962089766857858e-14.
Allowing negative dual variable(s) as small as -7.5767950941108e-14.
Allowing negative dual variable(s) as small as -1.4882279436578827e-13.
Allowing negative dual variable(s) as small as -1.4865712827383248e-13.
Solving took 4 GP solves and 1.66 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.258727481249892e-14.
Allowing negative dual variable(s) as small as -7.22976366274164e-14.
Allowing negative dual variable(s) as small as -1.4957132754567226e-13.
Allowing negative dual variable(s) as small as -1.493748701120179e-13.
Solving took 4 GP solves and 1.8 seconds.
Allowing negative dual variable(s) as small as -5.174489309256458e-13.
Allowing negative dual variable(s) as small as -1.4300054196336731e-12.
Allowing negative dual variable(s) as small as -4.4408574040311066e-13.
Allowing negative dual variable(s) as small as -4.456001539976384e-13.
Allowing negative dual variable(s) as small as -1.2982208624084945e-12.
Allowing negative dual variable(s) as small as -1.0920078860263138e-12.
Allowing negative dual variable(s) as small as -1.092428014368152e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4520314427108037e-14.
Allowing negative dual variable(s) as small as -5.696160623641188e-12.
Allowing negative dual variable(s) as small as -2.0878853075499786e-11.
Allowing negative dual variable(s) as small as -2.088100183595957e-11.
Solving took 4 GP solves and 1.38 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.18 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.158200255817036e-13.
Allowing negative dual variable(s) as small as -1.429642862427194e-12.
Allowing negative dual variable(s) as small as -4.4523239262073133e-13.
Allowing negative dual variable(s) as small as -4.454648455665122e-13.
Allowing negative dual variable(s) as small as -1.2983873958621883e-12.
Allowing negative dual variable(s) as small as -1.0914076717036258e-12.
Allowing negative dual variable(s) as small as -1.0904442496531552e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -2.241696411831029e-15.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.5223590424861995e-14.
Allowing negative dual variable(s) as small as -5.696115196337784e-12.
Allowing negative dual variable(s) as small as -2.087911214574125e-11.
Allowing negative dual variable(s) as small as -2.0880862737982447e-11.
Solving took 4 GP solves and 2.63 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.71 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error