Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180420092055)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.144526719711109e-14.
Allowing negative dual variable(s) as small as -8.368045839590721e-14.
Allowing negative dual variable(s) as small as -1.5152983035005008e-13.
Allowing negative dual variable(s) as small as -1.5370994407848393e-13.
Solving took 4 GP solves and 59.4 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.256503120085412e-14.
Allowing negative dual variable(s) as small as -8.186810604438044e-14.
Allowing negative dual variable(s) as small as -1.5046817958275227e-13.
Allowing negative dual variable(s) as small as -1.5418872775785353e-13.
Solving took 4 GP solves and 114 seconds.
Allowing negative dual variable(s) as small as -5.249307932775338e-13.
Allowing negative dual variable(s) as small as -5.101526839856874e-13.
Allowing negative dual variable(s) as small as -5.162311550455101e-13.
Allowing negative dual variable(s) as small as -5.147809262195935e-13.
Allowing negative dual variable(s) as small as -2.3860774467365786e-13.
Allowing negative dual variable(s) as small as -1.8787380505480566e-14.
Allowing negative dual variable(s) as small as -1.2598317571457796e-12.
Allowing negative dual variable(s) as small as -1.2592135450670283e-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 -2.0361750480146767e-14.
Allowing negative dual variable(s) as small as -1.137419151919783e-13.
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 -5.434127411921233e-11.
Allowing negative dual variable(s) as small as -6.449694179784765e-12.
Allowing negative dual variable(s) as small as -1.9339299839691406e-11.
Allowing negative dual variable(s) as small as -1.935456805249034e-11.
Solving took 4 GP solves and 30.7 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.93 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.238899591919477e-13.
Allowing negative dual variable(s) as small as -5.121632284943445e-13.
Allowing negative dual variable(s) as small as -5.164254440748195e-13.
Allowing negative dual variable(s) as small as -5.165989164224172e-13.
Allowing negative dual variable(s) as small as -2.386814704213869e-13.
Allowing negative dual variable(s) as small as -1.8969309630023634e-14.
Allowing negative dual variable(s) as small as -1.2602355140348132e-12.
Allowing negative dual variable(s) as small as -1.258303899444313e-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 -2.030537196717752e-14.
Allowing negative dual variable(s) as small as -1.139663450416828e-13.
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 -5.4341190329548516e-11.
Allowing negative dual variable(s) as small as -6.449652903339849e-12.
Allowing negative dual variable(s) as small as -1.9339201192328545e-11.
Allowing negative dual variable(s) as small as -1.935469502654078e-11.
Solving took 4 GP solves and 27.4 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 17.7 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error