Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180428095619)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.117646316084913e-14.
Allowing negative dual variable(s) as small as -7.779725214734912e-14.
Allowing negative dual variable(s) as small as -1.312812705767108e-13.
Allowing negative dual variable(s) as small as -1.2642762271114494e-13.
Solving took 4 GP solves and 6.35 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.61974034216295e-14.
Allowing negative dual variable(s) as small as -6.635599188176133e-14.
Allowing negative dual variable(s) as small as -1.3075727566674855e-13.
Allowing negative dual variable(s) as small as -1.2881286749061305e-13.
Solving took 4 GP solves and 7.62 seconds.
Allowing negative dual variable(s) as small as -5.850315891453572e-13.
Allowing negative dual variable(s) as small as -3.3793063833331694e-13.
Allowing negative dual variable(s) as small as -1.022974240039165e-12.
Allowing negative dual variable(s) as small as -1.022076086959478e-12.
Allowing negative dual variable(s) as small as -2.7603212684329526e-13.
Allowing negative dual variable(s) as small as -1.1550357024991964e-12.
Allowing negative dual variable(s) as small as -1.116510828019432e-12.
Allowing negative dual variable(s) as small as -1.1161072066556699e-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 -1.2095529113888281e-12.
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 -6.14544008971425e-11.
Allowing negative dual variable(s) as small as -1.4546773045318779e-12.
Allowing negative dual variable(s) as small as -6.463349134055873e-12.
Allowing negative dual variable(s) as small as -6.468851458228352e-12.
Solving took 4 GP solves and 5.89 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.3 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.844981616764944e-13.
Allowing negative dual variable(s) as small as -3.395027314834209e-13.
Allowing negative dual variable(s) as small as -1.0227972982446154e-12.
Allowing negative dual variable(s) as small as -1.0221402717280892e-12.
Allowing negative dual variable(s) as small as -2.7777937285436427e-13.
Allowing negative dual variable(s) as small as -1.1544863101533437e-12.
Allowing negative dual variable(s) as small as -1.1161437984789913e-12.
Allowing negative dual variable(s) as small as -1.1159076321407696e-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 -1.2093633928490777e-12.
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 -6.145438748797567e-11.
Allowing negative dual variable(s) as small as -1.4546608248573795e-12.
Allowing negative dual variable(s) as small as -6.463168154587613e-12.
Allowing negative dual variable(s) as small as -6.468772437320328e-12.
Solving took 4 GP solves and 5.8 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 3.36 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error