Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180104125859)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.64735324476e-13.
Allowing negative dual variable(s) as small as -6.33187079158e-13.
Allowing negative dual variable(s) as small as -7.39017571097e-13.
Allowing negative dual variable(s) as small as -1.83092278318e-12.
Solving took 4 GP solves and 6.56 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.69536605377e-13.
Allowing negative dual variable(s) as small as -1.4801057515e-12.
Allowing negative dual variable(s) as small as -9.07584988066e-13.
Allowing negative dual variable(s) as small as -8.70734690947e-13.
Solving took 4 GP solves and 9.53 seconds.
Allowing negative dual variable(s) as small as -9.28543266582e-14.
Allowing negative dual variable(s) as small as -6.00321760726e-10.
Allowing negative dual variable(s) as small as -4.38124607123e-13.
MTOW [lbs] = 132.53
Zero fuel weight [lbs] = 53.63
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.99015879731e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.76568314863e-12.
Allowing negative dual variable(s) as small as -2.89922219407e-12.
Allowing negative dual variable(s) as small as -4.21181139172e-12.
Allowing negative dual variable(s) as small as -4.21369135212e-12.
Solving took 4 GP solves and 2 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 2.42 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -9.11846553125e-14.
Allowing negative dual variable(s) as small as -6.0032203091e-10.
Allowing negative dual variable(s) as small as -4.39343304575e-13.
MTOW [lbs] = 132.53
Zero fuel weight [lbs] = 53.63
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -2.05999496974e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.7656160882e-12.
Allowing negative dual variable(s) as small as -2.89915574664e-12.
Allowing negative dual variable(s) as small as -4.21183681853e-12.
Allowing negative dual variable(s) as small as -4.21371901089e-12.
Solving took 4 GP solves and 2.18 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.93 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
	

Standard Error