Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180328102030)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.08212004266e-14.
Allowing negative dual variable(s) as small as -8.04872661575e-14.
Allowing negative dual variable(s) as small as -1.50118199121e-13.
Allowing negative dual variable(s) as small as -1.4885488675e-13.
Solving took 4 GP solves and 63.2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.01134332484e-14.
Allowing negative dual variable(s) as small as -8.0075269332e-14.
Allowing negative dual variable(s) as small as -1.52616634608e-13.
Allowing negative dual variable(s) as small as -1.48730854022e-13.
Solving took 4 GP solves and 20 seconds.
Allowing negative dual variable(s) as small as -5.23194335078e-13.
Allowing negative dual variable(s) as small as -5.13186715345e-13.
Allowing negative dual variable(s) as small as -5.1527532241e-13.
Allowing negative dual variable(s) as small as -5.16789736005e-13.
Allowing negative dual variable(s) as small as -2.33797356475e-13.
Allowing negative dual variable(s) as small as -1.87084505873e-14.
Allowing negative dual variable(s) as small as -1.25964516595e-12.
Allowing negative dual variable(s) as small as -1.25995329621e-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 -1.54702639588e-14.
Allowing negative dual variable(s) as small as -1.15198866071e-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 -5.43412102115e-11.
Allowing negative dual variable(s) as small as -6.4496174801e-12.
Allowing negative dual variable(s) as small as -1.93391138073e-11.
Allowing negative dual variable(s) as small as -1.9354643913e-11.
Solving took 4 GP solves and 23.1 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 9.44 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.23471890834e-13.
Allowing negative dual variable(s) as small as -5.12648951068e-13.
Allowing negative dual variable(s) as small as -5.13681111536e-13.
Allowing negative dual variable(s) as small as -5.16520853866e-13.
Allowing negative dual variable(s) as small as -2.36490514671e-13.
Allowing negative dual variable(s) as small as -1.94156756644e-14.
Allowing negative dual variable(s) as small as -1.26023659824e-12.
Allowing negative dual variable(s) as small as -1.25874918128e-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 -1.81564832613e-14.
Allowing negative dual variable(s) as small as -1.1343139969e-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 -5.43412621953e-11.
Allowing negative dual variable(s) as small as -6.44948819275e-12.
Allowing negative dual variable(s) as small as -1.93392508401e-11.
Allowing negative dual variable(s) as small as -1.93545675039e-11.
Solving took 4 GP solves and 13.7 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 9.06 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error