Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180420143705)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.9967100889362044e-14.
Allowing negative dual variable(s) as small as -3.262190864661285e-14.
Allowing negative dual variable(s) as small as -1.1624859061476478e-13.
Allowing negative dual variable(s) as small as -9.647447771210516e-14.
Solving took 4 GP solves and 5.26 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.3143379573875578e-14.
Allowing negative dual variable(s) as small as -3.9925528161344204e-14.
Allowing negative dual variable(s) as small as -1.2403229485147271e-13.
Allowing negative dual variable(s) as small as -7.766313633861266e-14.
Solving took 4 GP solves and 8.72 seconds.
Allowing negative dual variable(s) as small as -1.1891876372516208e-12.
Allowing negative dual variable(s) as small as -1.4595980674103615e-12.
Allowing negative dual variable(s) as small as -1.461721368944957e-12.
Allowing negative dual variable(s) as small as -2.56697441081144e-13.
Allowing negative dual variable(s) as small as -1.3360838043569023e-12.
Allowing negative dual variable(s) as small as -1.2347347536773023e-12.
Allowing negative dual variable(s) as small as -1.234860195868659e-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 -3.942159099157294e-14.
Allowing negative dual variable(s) as small as -2.0248299564817884e-13.
Allowing negative dual variable(s) as small as -2.0333409435357996e-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 -7.954841949744744e-15.
Allowing negative dual variable(s) as small as -4.073320671034836e-12.
Allowing negative dual variable(s) as small as -2.2201981580755713e-11.
Allowing negative dual variable(s) as small as -2.2195679782524264e-11.
Solving took 4 GP solves and 4.74 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 2.32 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -1.1905528646272145e-12.
Allowing negative dual variable(s) as small as -1.460311038758988e-12.
Allowing negative dual variable(s) as small as -1.4608817627825843e-12.
Allowing negative dual variable(s) as small as -2.5625335187129394e-13.
Allowing negative dual variable(s) as small as -1.3357500869282113e-12.
Allowing negative dual variable(s) as small as -1.2354446892598459e-12.
Allowing negative dual variable(s) as small as -1.2349097439079415e-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 -3.662131362047738e-14.
Allowing negative dual variable(s) as small as -2.0249188610599322e-13.
Allowing negative dual variable(s) as small as -2.03256031797161e-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 -8.960550531920259e-15.
Allowing negative dual variable(s) as small as -4.073203468144715e-12.
Allowing negative dual variable(s) as small as -2.2202017373932844e-11.
Allowing negative dual variable(s) as small as -2.219564027251362e-11.
Solving took 4 GP solves and 3.4 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 5.4 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error