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Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171110160150)

Took 16 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.06817766438e-13.
Allowing negative dual variable(s) as small as -1.11046588591e-13.
Allowing negative dual variable(s) as small as -6.02816407902e-17.
Solving took 4 GP solves and 1.94 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.12305564154e-13.
Allowing negative dual variable(s) as small as -1.04804619844e-13.
Allowing negative dual variable(s) as small as -1.78242837157e-16.
Solving took 4 GP solves and 1.96 seconds.
Allowing negative dual variable(s) as small as -3.88110810851e-12.
Allowing negative dual variable(s) as small as -1.71202114985e-12.
Allowing negative dual variable(s) as small as -7.75747521775e-13.
Allowing negative dual variable(s) as small as -7.69812165402e-13.
Allowing negative dual variable(s) as small as -7.70280540741e-13.
Allowing negative dual variable(s) as small as -2.50669927523e-13.
Allowing negative dual variable(s) as small as -1.01755366286e-12.
Allowing negative dual variable(s) as small as -1.05833495179e-12.
Allowing negative dual variable(s) as small as -1.04851977795e-12.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.57916518004e-13.
Allowing negative dual variable(s) as small as -1.4807653801e-13.
Allowing negative dual variable(s) as small as -1.47298080851e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.00724955139e-13.
Allowing negative dual variable(s) as small as -1.99596415996e-15.
Allowing negative dual variable(s) as small as -8.98273020082e-14.
Allowing negative dual variable(s) as small as -8.83491356004e-14.
Solving took 4 GP solves and 2.68 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.6 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88079152147e-12.
Allowing negative dual variable(s) as small as -1.71216686662e-12.
Allowing negative dual variable(s) as small as -7.75202818604e-13.
Allowing negative dual variable(s) as small as -7.70398501937e-13.
Allowing negative dual variable(s) as small as -7.69859870298e-13.
Allowing negative dual variable(s) as small as -2.47232789796e-13.
Allowing negative dual variable(s) as small as -1.01844064865e-12.
Allowing negative dual variable(s) as small as -1.05768269577e-12.
Allowing negative dual variable(s) as small as -1.04880817572e-12.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.59545857029e-13.
Allowing negative dual variable(s) as small as -1.48426843732e-13.
Allowing negative dual variable(s) as small as -1.47245930726e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.0015814589e-13.
Allowing negative dual variable(s) as small as -1.79841813015e-15.
Allowing negative dual variable(s) as small as -8.76431936194e-14.
Allowing negative dual variable(s) as small as -8.78198140179e-14.
Solving took 4 GP solves and 2.64 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.65 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error