Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428145015)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.219739571127313e-14.
Allowing negative dual variable(s) as small as -7.455277714618624e-14.
Allowing negative dual variable(s) as small as -1.5124143257216893e-13.
Allowing negative dual variable(s) as small as -1.5034197844987496e-13.
Solving took 4 GP solves and 1.49 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -4.976791548316761e-14.
Allowing negative dual variable(s) as small as -7.349589686844737e-14.
Allowing negative dual variable(s) as small as -1.4906565565242502e-13.
Allowing negative dual variable(s) as small as -1.4885445306922485e-13.
Solving took 4 GP solves and 2.66 seconds.
Allowing negative dual variable(s) as small as -5.188054846838597e-13.
Allowing negative dual variable(s) as small as -1.4305084894417064e-12.
Allowing negative dual variable(s) as small as -4.443008461141318e-13.
Allowing negative dual variable(s) as small as -4.433640954371043e-13.
Allowing negative dual variable(s) as small as -1.2970375641574439e-12.
Allowing negative dual variable(s) as small as -1.090706301318245e-12.
Allowing negative dual variable(s) as small as -1.0900240128910998e-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 -2.4208442189884924e-14.
Allowing negative dual variable(s) as small as -5.696078658777511e-12.
Allowing negative dual variable(s) as small as -2.087891440169102e-11.
Allowing negative dual variable(s) as small as -2.088077509249231e-11.
Solving took 4 GP solves and 1.85 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.79 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.176553630192871e-13.
Allowing negative dual variable(s) as small as -1.4304200185444316e-12.
Allowing negative dual variable(s) as small as -4.4475187421788576e-13.
Allowing negative dual variable(s) as small as -4.4558107203940267e-13.
Allowing negative dual variable(s) as small as -1.296803376488187e-12.
Allowing negative dual variable(s) as small as -1.0926626357182778e-12.
Allowing negative dual variable(s) as small as -1.0907542230542688e-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 -2.497929712314879e-14.
Allowing negative dual variable(s) as small as -5.696092591887158e-12.
Allowing negative dual variable(s) as small as -2.0879010539454076e-11.
Allowing negative dual variable(s) as small as -2.0881047093512277e-11.
Solving took 4 GP solves and 2.07 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.48 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error