Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180327110942)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.94854633501263e-14.
Allowing negative dual variable(s) as small as -8.094696787863676e-14.
Allowing negative dual variable(s) as small as -1.4931111902427574e-13.
Allowing negative dual variable(s) as small as -1.5455301968780866e-13.
Solving took 4 GP solves and 3.38 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.115209892967101e-14.
Allowing negative dual variable(s) as small as -8.039966262196607e-14.
Allowing negative dual variable(s) as small as -1.5334218270157685e-13.
Allowing negative dual variable(s) as small as -1.5367828537504735e-13.
Solving took 4 GP solves and 3.11 seconds.
Allowing negative dual variable(s) as small as -5.23194335078081e-13.
Allowing negative dual variable(s) as small as -5.119672047415591e-13.
Allowing negative dual variable(s) as small as -5.13922238098985e-13.
Allowing negative dual variable(s) as small as -5.160802341031001e-13.
Allowing negative dual variable(s) as small as -2.3982855631987654e-13.
Allowing negative dual variable(s) as small as -1.8032016851909916e-14.
Allowing negative dual variable(s) as small as -1.2600129273288019e-12.
Allowing negative dual variable(s) as small as -1.2603232259905672e-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 -2.0726909771839885e-14.
Allowing negative dual variable(s) as small as -1.1292204150914475e-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 -5.4341288155501176e-11.
Allowing negative dual variable(s) as small as -6.449674123950398e-12.
Allowing negative dual variable(s) as small as -1.933933023287468e-11.
Allowing negative dual variable(s) as small as -1.935451674680475e-11.
Solving took 4 GP solves and 2.76 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.69 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.225351401572098e-13.
Allowing negative dual variable(s) as small as -5.111952527947494e-13.
Allowing negative dual variable(s) as small as -5.128935470777307e-13.
Allowing negative dual variable(s) as small as -5.144704107173936e-13.
Allowing negative dual variable(s) as small as -2.373925708787361e-13.
Allowing negative dual variable(s) as small as -1.7858652924529483e-14.
Allowing negative dual variable(s) as small as -1.2604882415612195e-12.
Allowing negative dual variable(s) as small as -1.2590710809015637e-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 -1.688796671950321e-14.
Allowing negative dual variable(s) as small as -1.1349580129882408e-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 -5.434124927965351e-11.
Allowing negative dual variable(s) as small as -6.449684985903867e-12.
Allowing negative dual variable(s) as small as -1.9339260045660028e-11.
Allowing negative dual variable(s) as small as -1.9354687338393295e-11.
Solving took 4 GP solves and 2.92 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.73 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error