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Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180420100244)

Took 18 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.237854842718662e-14.
Allowing negative dual variable(s) as small as -8.269600282329037e-14.
Allowing negative dual variable(s) as small as -1.4942908022064216e-13.
Allowing negative dual variable(s) as small as -1.4790599300873453e-13.
Solving took 4 GP solves and 3.33 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.940479870849337e-14.
Allowing negative dual variable(s) as small as -8.395411102424255e-14.
Allowing negative dual variable(s) as small as -1.5144266049538224e-13.
Allowing negative dual variable(s) as small as -1.472806251956449e-13.
Solving took 4 GP solves and 3.42 seconds.
Allowing negative dual variable(s) as small as -5.226964694404757e-13.
Allowing negative dual variable(s) as small as -5.124060897809812e-13.
Allowing negative dual variable(s) as small as -5.151538917669285e-13.
Allowing negative dual variable(s) as small as -5.144704107173936e-13.
Allowing negative dual variable(s) as small as -2.353885315831139e-13.
Allowing negative dual variable(s) as small as -1.8174264176940014e-14.
Allowing negative dual variable(s) as small as -1.2596135072484582e-12.
Allowing negative dual variable(s) as small as -1.2595466119744159e-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 -2.0022612040593302e-14.
Allowing negative dual variable(s) as small as -1.1358687428131287e-13.
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 -5.434120119189903e-11.
Allowing negative dual variable(s) as small as -6.449757292977288e-12.
Allowing negative dual variable(s) as small as -1.9339270377317932e-11.
Allowing negative dual variable(s) as small as -1.935458917312453e-11.
Solving took 4 GP solves and 3.34 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.23 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.234736255577133e-13.
Allowing negative dual variable(s) as small as -5.11977613082415e-13.
Allowing negative dual variable(s) as small as -5.139794839736922e-13.
Allowing negative dual variable(s) as small as -5.151469528730246e-13.
Allowing negative dual variable(s) as small as -2.3357617923158713e-13.
Allowing negative dual variable(s) as small as -1.8523485696697595e-14.
Allowing negative dual variable(s) as small as -1.259630420802349e-12.
Allowing negative dual variable(s) as small as -1.2604018306480724e-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 -1.9057672107081203e-14.
Allowing negative dual variable(s) as small as -1.138087020458034e-13.
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 -5.434122263591452e-11.
Allowing negative dual variable(s) as small as -6.449648495327452e-12.
Allowing negative dual variable(s) as small as -1.933929786583994e-11.
Allowing negative dual variable(s) as small as -1.9354637164343725e-11.
Solving took 4 GP solves and 3.01 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.25 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error