Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180605094814)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.791434598197755e-14.
Allowing negative dual variable(s) as small as -7.259178067681171e-14.
Allowing negative dual variable(s) as small as -2.574325301540892e-13.
Allowing negative dual variable(s) as small as -1.295834099745985e-13.
Solving took 4 GP solves and 1.23 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.791434598197755e-14.
Allowing negative dual variable(s) as small as -7.259178067681171e-14.
Allowing negative dual variable(s) as small as -2.574325301540892e-13.
Allowing negative dual variable(s) as small as -1.295834099745985e-13.
Solving took 4 GP solves and 1.41 seconds.
Allowing negative dual variable(s) as small as -5.853030733693476e-13.
Allowing negative dual variable(s) as small as -3.3867049789582104e-13.
Allowing negative dual variable(s) as small as -1.0218830989727756e-12.
Allowing negative dual variable(s) as small as -1.0211662244963282e-12.
Allowing negative dual variable(s) as small as -2.713894647204951e-13.
Allowing negative dual variable(s) as small as -1.1530335063472674e-12.
Allowing negative dual variable(s) as small as -1.1157666587532922e-12.
Allowing negative dual variable(s) as small as -1.1156585909017497e-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 -1.2096535795605434e-12.
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 -6.145426241487892e-11.
Allowing negative dual variable(s) as small as -1.454814909891364e-12.
Allowing negative dual variable(s) as small as -6.4633620051979626e-12.
Allowing negative dual variable(s) as small as -6.469039237200657e-12.
Solving took 4 GP solves and 1.25 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.08 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.853030733693476e-13.
Allowing negative dual variable(s) as small as -3.3867049789582104e-13.
Allowing negative dual variable(s) as small as -1.0218830989727756e-12.
Allowing negative dual variable(s) as small as -1.0211662244963282e-12.
Allowing negative dual variable(s) as small as -2.713894647204951e-13.
Allowing negative dual variable(s) as small as -1.1530335063472674e-12.
Allowing negative dual variable(s) as small as -1.1157666587532922e-12.
Allowing negative dual variable(s) as small as -1.1156585909017497e-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 -1.2096535795605434e-12.
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 -6.145426241487892e-11.
Allowing negative dual variable(s) as small as -1.454814909891364e-12.
Allowing negative dual variable(s) as small as -6.4633620051979626e-12.
Allowing negative dual variable(s) as small as -6.469039237200657e-12.
Solving took 4 GP solves and 1.49 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.29 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error