Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180420093144)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.070757603895196e-14.
Allowing negative dual variable(s) as small as -8.167338333420204e-14.
Allowing negative dual variable(s) as small as -1.5013294427101975e-13.
Allowing negative dual variable(s) as small as -1.498523527487805e-13.
Solving took 4 GP solves and 22.7 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.092615119692503e-14.
Allowing negative dual variable(s) as small as -8.331313069986912e-14.
Allowing negative dual variable(s) as small as -1.4854827437571494e-13.
Allowing negative dual variable(s) as small as -1.5035585623768277e-13.
Solving took 4 GP solves and 25.9 seconds.
Allowing negative dual variable(s) as small as -5.245769096884345e-13.
Allowing negative dual variable(s) as small as -5.133411057345327e-13.
Allowing negative dual variable(s) as small as -5.157489019191885e-13.
Allowing negative dual variable(s) as small as -5.160958466143839e-13.
Allowing negative dual variable(s) as small as -2.3804786267178635e-13.
Allowing negative dual variable(s) as small as -1.9255647423777056e-14.
Allowing negative dual variable(s) as small as -1.2582259453081113e-12.
Allowing negative dual variable(s) as small as -1.2602281414600403e-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 -1.975806671050684e-14.
Allowing negative dual variable(s) as small as -1.134721656914639e-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 -5.434126862779185e-11.
Allowing negative dual variable(s) as small as -6.449560335688316e-12.
Allowing negative dual variable(s) as small as -1.933920869309646e-11.
Allowing negative dual variable(s) as small as -1.9354706988948867e-11.
Solving took 4 GP solves and 10.3 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 9.58 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.238101619120528e-13.
Allowing negative dual variable(s) as small as -5.126749719197576e-13.
Allowing negative dual variable(s) as small as -5.146594955762751e-13.
Allowing negative dual variable(s) as small as -5.169441263941366e-13.
Allowing negative dual variable(s) as small as -2.3776987323476106e-13.
Allowing negative dual variable(s) as small as -1.8218933306446417e-14.
Allowing negative dual variable(s) as small as -1.2604569081184347e-12.
Allowing negative dual variable(s) as small as -1.259798363718867e-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 -2.3087434741775326e-14.
Allowing negative dual variable(s) as small as -1.1394617888127456e-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 -5.4341336308265437e-11.
Allowing negative dual variable(s) as small as -6.449682554310503e-12.
Allowing negative dual variable(s) as small as -1.9339259673706685e-11.
Allowing negative dual variable(s) as small as -1.9354613560738328e-11.
Solving took 4 GP solves and 17.2 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 5.48 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error