Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171112202811)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.61036851856e-13.
Allowing negative dual variable(s) as small as -9.2916126182e-14.
Allowing negative dual variable(s) as small as -2.51369758342e-12.
Allowing negative dual variable(s) as small as -2.47040148754e-12.
Solving took 4 GP solves and 2.34 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.61036851856e-13.
Allowing negative dual variable(s) as small as -9.2916126182e-14.
Allowing negative dual variable(s) as small as -2.51369758342e-12.
Allowing negative dual variable(s) as small as -2.47040148754e-12.
Solving took 4 GP solves and 2.58 seconds.
Allowing negative dual variable(s) as small as -3.60041423758e-12.
Allowing negative dual variable(s) as small as -1.58857475785e-12.
Allowing negative dual variable(s) as small as -1.77729185535e-12.
Allowing negative dual variable(s) as small as -7.78800635093e-13.
Allowing negative dual variable(s) as small as -7.78106745702e-13.
Allowing negative dual variable(s) as small as -2.76403682928e-13.
Allowing negative dual variable(s) as small as -1.0992029769e-12.
Allowing negative dual variable(s) as small as -1.06869406987e-12.
Allowing negative dual variable(s) as small as -1.06195434391e-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 -2.27370596309e-12.
Allowing negative dual variable(s) as small as -7.2326367985e-14.
Allowing negative dual variable(s) as small as -1.20836825789e-13.
Allowing negative dual variable(s) as small as -1.20700433155e-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 -2.64087058162e-12.
Allowing negative dual variable(s) as small as -1.98068463003e-12.
Allowing negative dual variable(s) as small as -1.9965789459e-12.
Solving took 4 GP solves and 2.41 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.85058911839e-12.
Solving took 4 GP solves and 1.26 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.60041423758e-12.
Allowing negative dual variable(s) as small as -1.58857475785e-12.
Allowing negative dual variable(s) as small as -1.77729185535e-12.
Allowing negative dual variable(s) as small as -7.78800635093e-13.
Allowing negative dual variable(s) as small as -7.78106745702e-13.
Allowing negative dual variable(s) as small as -2.76403682928e-13.
Allowing negative dual variable(s) as small as -1.0992029769e-12.
Allowing negative dual variable(s) as small as -1.06869406987e-12.
Allowing negative dual variable(s) as small as -1.06195434391e-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 -2.27370596309e-12.
Allowing negative dual variable(s) as small as -7.2326367985e-14.
Allowing negative dual variable(s) as small as -1.20836825789e-13.
Allowing negative dual variable(s) as small as -1.20700433155e-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 -2.64087058162e-12.
Allowing negative dual variable(s) as small as -1.98068463003e-12.
Allowing negative dual variable(s) as small as -1.9965789459e-12.
Solving took 4 GP solves and 2.48 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.85058911839e-12.
Solving took 4 GP solves and 1.87 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error