Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180124112821)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -6.39124170254135e-14.
Allowing negative dual variable(s) as small as -1.6628148510888785e-13.
Allowing negative dual variable(s) as small as -2.5674774806194733e-14.
Allowing negative dual variable(s) as small as -2.105260410445453e-14.
Solving took 4 GP solves and 21.8 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.630280533990394e-14.
Allowing negative dual variable(s) as small as -8.351305758047545e-14.
Allowing negative dual variable(s) as small as -2.4971344436686138e-14.
Allowing negative dual variable(s) as small as -3.322038824582485e-14.
Solving took 4 GP solves and 7.7 seconds.
Allowing negative dual variable(s) as small as -1.473690960929197e-13.
Allowing negative dual variable(s) as small as -1.429571738764679e-12.
Allowing negative dual variable(s) as small as -1.2564532747560975e-12.
Allowing negative dual variable(s) as small as -1.2561991377668669e-12.
Allowing negative dual variable(s) as small as -1.43397793639366e-12.
Allowing negative dual variable(s) as small as -1.761468358327245e-12.
Allowing negative dual variable(s) as small as -1.745869074309958e-13.
Allowing negative dual variable(s) as small as -2.3455326222943107e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.2262456675071753e-12.
Allowing negative dual variable(s) as small as -1.7237925496738082e-13.
Allowing negative dual variable(s) as small as -5.1057248706687375e-14.
Allowing negative dual variable(s) as small as -5.689762896943229e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.4887502616434006e-11.
Allowing negative dual variable(s) as small as -1.8840388768816714e-12.
Allowing negative dual variable(s) as small as -2.843121761492079e-12.
Allowing negative dual variable(s) as small as -2.841795439623537e-12.
Solving took 4 GP solves and 10.9 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.0469806405465363e-12.
Solving took 4 GP solves and 1.7 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
Allowing negative dual variable(s) as small as -1.475642524839671e-13.
Allowing negative dual variable(s) as small as -1.4299160813746603e-12.
Allowing negative dual variable(s) as small as -1.2559155104785447e-12.
Allowing negative dual variable(s) as small as -1.256108064784378e-12.
Allowing negative dual variable(s) as small as -1.4348188435986398e-12.
Allowing negative dual variable(s) as small as -1.7638854786505842e-12.
Allowing negative dual variable(s) as small as -1.788662534057961e-13.
Allowing negative dual variable(s) as small as -2.376861728270452e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.2247115214331084e-12.
Allowing negative dual variable(s) as small as -1.719989168452729e-13.
Allowing negative dual variable(s) as small as -5.051905074826557e-14.
Allowing negative dual variable(s) as small as -5.475329391269046e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.488747944588744e-11.
Allowing negative dual variable(s) as small as -1.8838519056049126e-12.
Allowing negative dual variable(s) as small as -2.843212825676675e-12.
Allowing negative dual variable(s) as small as -2.8416700327924973e-12.
Solving took 4 GP solves and 3.73 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.049907119050509e-12.
Solving took 4 GP solves and 27.6 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
	

Standard Error