Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180430090758)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.187733922995541e-14.
Allowing negative dual variable(s) as small as -7.610275257197152e-14.
Allowing negative dual variable(s) as small as -1.5324373714431516e-13.
Allowing negative dual variable(s) as small as -1.490530789072242e-13.
Solving took 4 GP solves and 1.52 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.1685652285859973e-14.
Allowing negative dual variable(s) as small as -7.617387623448657e-14.
Allowing negative dual variable(s) as small as -1.5193662300516664e-13.
Allowing negative dual variable(s) as small as -1.4918491789139843e-13.
Solving took 4 GP solves and 1.56 seconds.
Allowing negative dual variable(s) as small as -5.164809552260508e-13.
Allowing negative dual variable(s) as small as -1.4290929550853093e-12.
Allowing negative dual variable(s) as small as -4.425279587216835e-13.
Allowing negative dual variable(s) as small as -4.4369716234449186e-13.
Allowing negative dual variable(s) as small as -1.296461419122985e-12.
Allowing negative dual variable(s) as small as -1.0906043863140313e-12.
Allowing negative dual variable(s) as small as -1.0897607686036204e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.3673957799387182e-15.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.269
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4224887546314103e-14.
Allowing negative dual variable(s) as small as -5.695991936420937e-12.
Allowing negative dual variable(s) as small as -2.0878956261953393e-11.
Allowing negative dual variable(s) as small as -2.08809198198504e-11.
Solving took 4 GP solves and 9.07 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.11 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.181636369977483e-13.
Allowing negative dual variable(s) as small as -1.4313307483693194e-12.
Allowing negative dual variable(s) as small as -4.440527806570671e-13.
Allowing negative dual variable(s) as small as -4.4303276325319274e-13.
Allowing negative dual variable(s) as small as -1.2955936237041277e-12.
Allowing negative dual variable(s) as small as -1.089524195689584e-12.
Allowing negative dual variable(s) as small as -1.0905650297751701e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 25.637
optimum cruise speed, outbound [m/s] = 36.269
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.452211458387919e-14.
Allowing negative dual variable(s) as small as -5.695964096009678e-12.
Allowing negative dual variable(s) as small as -2.0878974455241718e-11.
Allowing negative dual variable(s) as small as -2.0880738988639375e-11.
Solving took 4 GP solves and 1.65 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.3 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error