Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171110172230)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.11233071365e-13.
Allowing negative dual variable(s) as small as -1.07086648576e-13.
Allowing negative dual variable(s) as small as -1.69135538908e-16.
Allowing negative dual variable(s) as small as -9.10729824888e-18.
Solving took 4 GP solves and 1.48 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.15190409294e-13.
Allowing negative dual variable(s) as small as -1.06298650437e-13.
Allowing negative dual variable(s) as small as -1.30537941567e-16.
Solving took 4 GP solves and 2.16 seconds.
Allowing negative dual variable(s) as small as -3.88170919019e-12.
Allowing negative dual variable(s) as small as -1.71183987124e-12.
Allowing negative dual variable(s) as small as -7.74815975269e-13.
Allowing negative dual variable(s) as small as -7.70217223334e-13.
Allowing negative dual variable(s) as small as -7.7029008172e-13.
Allowing negative dual variable(s) as small as -2.51234580015e-13.
Allowing negative dual variable(s) as small as -1.01709276851e-12.
Allowing negative dual variable(s) as small as -1.05768583995e-12.
Allowing negative dual variable(s) as small as -1.04757825678e-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 -2.57218074964e-13.
Allowing negative dual variable(s) as small as -1.48769017938e-13.
Allowing negative dual variable(s) as small as -1.46587820007e-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 -4.00544577356e-13.
Allowing negative dual variable(s) as small as -1.59692111516e-15.
Allowing negative dual variable(s) as small as -8.77897784943e-14.
Allowing negative dual variable(s) as small as -8.81360655743e-14.
Solving took 4 GP solves and 1.72 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.3 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88189133615e-12.
Allowing negative dual variable(s) as small as -1.71161956136e-12.
Allowing negative dual variable(s) as small as -7.75199349157e-13.
Allowing negative dual variable(s) as small as -7.69894564767e-13.
Allowing negative dual variable(s) as small as -7.7025018308e-13.
Allowing negative dual variable(s) as small as -2.49138817215e-13.
Allowing negative dual variable(s) as small as -1.01531511063e-12.
Allowing negative dual variable(s) as small as -1.05791623291e-12.
Allowing negative dual variable(s) as small as -1.04711898874e-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 -2.61994852896e-13.
Allowing negative dual variable(s) as small as -1.47145316765e-13.
Allowing negative dual variable(s) as small as -1.47087095108e-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 -4.00087030063e-13.
Allowing negative dual variable(s) as small as -8.61923828289e-14.
Allowing negative dual variable(s) as small as -8.8533558337e-14.
Solving took 4 GP solves and 21.3 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.33 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error