Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428095413)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.354137272428616e-14.
Allowing negative dual variable(s) as small as -7.20578111068626e-14.
Allowing negative dual variable(s) as small as -1.5073619435979069e-13.
Allowing negative dual variable(s) as small as -1.49666303655982e-13.
Solving took 4 GP solves and 2.25 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.145623510616204e-14.
Allowing negative dual variable(s) as small as -7.336882837383207e-14.
Allowing negative dual variable(s) as small as -1.5158317309693636e-13.
Allowing negative dual variable(s) as small as -1.4994559413561426e-13.
Solving took 4 GP solves and 2.04 seconds.
Allowing negative dual variable(s) as small as -5.170343320148874e-13.
Allowing negative dual variable(s) as small as -1.4290253008697462e-12.
Allowing negative dual variable(s) as small as -4.444500323330658e-13.
Allowing negative dual variable(s) as small as -4.429252103976822e-13.
Allowing negative dual variable(s) as small as -1.2963273033142486e-12.
Allowing negative dual variable(s) as small as -1.09193513606054e-12.
Allowing negative dual variable(s) as small as -1.090718119121925e-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 -1.7468665403086447e-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] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4513905564070874e-14.
Allowing negative dual variable(s) as small as -5.695945464275923e-12.
Allowing negative dual variable(s) as small as -2.0878982722230344e-11.
Allowing negative dual variable(s) as small as -2.0880777230932864e-11.
Solving took 4 GP solves and 1.93 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.37 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.171939265746772e-13.
Allowing negative dual variable(s) as small as -1.430086951637044e-12.
Allowing negative dual variable(s) as small as -4.4500687856885435e-13.
Allowing negative dual variable(s) as small as -4.448542229029684e-13.
Allowing negative dual variable(s) as small as -1.2989366526827695e-12.
Allowing negative dual variable(s) as small as -1.0909718224302867e-12.
Allowing negative dual variable(s) as small as -1.0904557421961836e-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] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.4278882614448894e-14.
Allowing negative dual variable(s) as small as -5.696087727694579e-12.
Allowing negative dual variable(s) as small as -2.087882565391985e-11.
Allowing negative dual variable(s) as small as -2.088087791710403e-11.
Solving took 4 GP solves and 1.57 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.58 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error