Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171110171557)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.11153274085e-13.
Allowing negative dual variable(s) as small as -1.06380616122e-13.
Allowing negative dual variable(s) as small as -1.43114686768e-17.
Solving took 4 GP solves and 1.86 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.11107303913e-13.
Allowing negative dual variable(s) as small as -1.09390361352e-13.
Allowing negative dual variable(s) as small as -9.84455572617e-17.
Allowing negative dual variable(s) as small as -1.51354623279e-16.
Solving took 4 GP solves and 1.71 seconds.
Allowing negative dual variable(s) as small as -3.8805868241e-12.
Allowing negative dual variable(s) as small as -1.7126682017e-12.
Allowing negative dual variable(s) as small as -7.74969498296e-13.
Allowing negative dual variable(s) as small as -7.69244910825e-13.
Allowing negative dual variable(s) as small as -7.6944180194e-13.
Allowing negative dual variable(s) as small as -2.54615122389e-13.
Allowing negative dual variable(s) as small as -1.01664119831e-12.
Allowing negative dual variable(s) as small as -1.0585355292e-12.
Allowing negative dual variable(s) as small as -1.04666427435e-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 -2.56106550897e-13.
Allowing negative dual variable(s) as small as -1.47749434215e-13.
Allowing negative dual variable(s) as small as -1.47571408218e-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 -4.00590630325e-13.
Allowing negative dual variable(s) as small as -2.35824459842e-15.
Allowing negative dual variable(s) as small as -8.72990549326e-14.
Allowing negative dual variable(s) as small as -8.91283702836e-14.
Solving took 4 GP solves and 2.7 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.43 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88049575112e-12.
Allowing negative dual variable(s) as small as -1.7128564192e-12.
Allowing negative dual variable(s) as small as -7.75346800652e-13.
Allowing negative dual variable(s) as small as -7.69756654251e-13.
Allowing negative dual variable(s) as small as -7.6988589115e-13.
Allowing negative dual variable(s) as small as -2.46280426608e-13.
Allowing negative dual variable(s) as small as -1.01719164775e-12.
Allowing negative dual variable(s) as small as -1.05702089876e-12.
Allowing negative dual variable(s) as small as -1.04712874656e-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 -2.61804683835e-13.
Allowing negative dual variable(s) as small as -1.47199418453e-13.
Allowing negative dual variable(s) as small as -1.47507765551e-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 -4.00745112194e-13.
Allowing negative dual variable(s) as small as -4.09794010486e-16.
Allowing negative dual variable(s) as small as -9.09910495212e-14.
Allowing negative dual variable(s) as small as -8.80209226683e-14.
Solving took 4 GP solves and 2.49 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.59 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error