Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171111180053)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.09601997617e-13.
Allowing negative dual variable(s) as small as -1.07259687243e-13.
Allowing negative dual variable(s) as small as -2.60642202266e-16.
Solving took 4 GP solves and 41.4 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.11761294663e-13.
Allowing negative dual variable(s) as small as -1.07669081983e-13.
Allowing negative dual variable(s) as small as -1.12757025938e-17.
Allowing negative dual variable(s) as small as -1.40946282423e-16.
Solving took 4 GP solves and 47.1 seconds.
Allowing negative dual variable(s) as small as -3.88171092491e-12.
Allowing negative dual variable(s) as small as -1.71191619908e-12.
Allowing negative dual variable(s) as small as -7.75272207543e-13.
Allowing negative dual variable(s) as small as -7.70128752436e-13.
Allowing negative dual variable(s) as small as -7.70108803116e-13.
Allowing negative dual variable(s) as small as -2.51478091823e-13.
Allowing negative dual variable(s) as small as -1.01611893812e-12.
Allowing negative dual variable(s) as small as -1.05758078076e-12.
Allowing negative dual variable(s) as small as -1.0464494939e-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 -2.60628324478e-13.
Allowing negative dual variable(s) as small as -1.46666099404e-13.
Allowing negative dual variable(s) as small as -1.47121247476e-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 -4.00354200136e-13.
Allowing negative dual variable(s) as small as -1.62090982938e-15.
Allowing negative dual variable(s) as small as -8.88461295882e-14.
Allowing negative dual variable(s) as small as -8.6591123483e-14.
Solving took 4 GP solves and 33 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 32 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88172133325e-12.
Allowing negative dual variable(s) as small as -1.71232559382e-12.
Allowing negative dual variable(s) as small as -7.75535018149e-13.
Allowing negative dual variable(s) as small as -7.70092323243e-13.
Allowing negative dual variable(s) as small as -7.70264928229e-13.
Allowing negative dual variable(s) as small as -2.51057855061e-13.
Allowing negative dual variable(s) as small as -1.01587195687e-12.
Allowing negative dual variable(s) as small as -1.05762132992e-12.
Allowing negative dual variable(s) as small as -1.0473965445e-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 -2.60222832865e-13.
Allowing negative dual variable(s) as small as -1.47556337808e-13.
Allowing negative dual variable(s) as small as -1.46537404606e-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 -4.00266403477e-13.
Allowing negative dual variable(s) as small as -3.95389352303e-15.
Allowing negative dual variable(s) as small as -8.85382534936e-14.
Allowing negative dual variable(s) as small as -8.82124546054e-14.
Solving took 4 GP solves and 30.2 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 24.5 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error