Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171101154348)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.71845913436e-12.
Allowing negative dual variable(s) as small as -1.87220633961e-11.
Allowing negative dual variable(s) as small as -3.62182072527e-13.
Allowing negative dual variable(s) as small as -4.61109015554e-13.
Solving took 4 GP solves and 1.38 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.71845913436e-12.
Allowing negative dual variable(s) as small as -1.87220633961e-11.
Allowing negative dual variable(s) as small as -3.62182072527e-13.
Allowing negative dual variable(s) as small as -4.61109015554e-13.
Solving took 4 GP solves and 1.19 seconds.
Allowing negative dual variable(s) as small as -2.31380123394e-11.
Allowing negative dual variable(s) as small as -8.79610967397e-12.
Allowing negative dual variable(s) as small as -1.98742064472e-11.
Allowing negative dual variable(s) as small as -7.68574787147e-12.
Allowing negative dual variable(s) as small as -7.66163521515e-12.
Allowing negative dual variable(s) as small as -2.36046358241e-11.
Allowing negative dual variable(s) as small as -1.17887586628e-11.
Allowing negative dual variable(s) as small as -1.1977331453e-11.
Allowing negative dual variable(s) as small as -1.17717234615e-11.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.73221625446e-11.
Allowing negative dual variable(s) as small as -1.24184061472e-11.
Allowing negative dual variable(s) as small as -7.11262754423e-12.
Allowing negative dual variable(s) as small as -6.64457584006e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.45685117514e-12.
Allowing negative dual variable(s) as small as -2.4004082752e-12.
Allowing negative dual variable(s) as small as -7.67767478698e-11.
Allowing negative dual variable(s) as small as -8.54843495689e-11.
Solving took 4 GP solves and 2.58 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93834314119e-12.
Allowing negative dual variable(s) as small as -3.89277473103e-11.
Allowing negative dual variable(s) as small as -5.41168030527e-11.
Allowing negative dual variable(s) as small as -5.45077355647e-11.
Solving took 4 GP solves and 2.01 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.31380123394e-11.
Allowing negative dual variable(s) as small as -8.79610967397e-12.
Allowing negative dual variable(s) as small as -1.98742064472e-11.
Allowing negative dual variable(s) as small as -7.68574787147e-12.
Allowing negative dual variable(s) as small as -7.66163521515e-12.
Allowing negative dual variable(s) as small as -2.36046358241e-11.
Allowing negative dual variable(s) as small as -1.17887586628e-11.
Allowing negative dual variable(s) as small as -1.1977331453e-11.
Allowing negative dual variable(s) as small as -1.17717234615e-11.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.73221625446e-11.
Allowing negative dual variable(s) as small as -1.24184061472e-11.
Allowing negative dual variable(s) as small as -7.11262754423e-12.
Allowing negative dual variable(s) as small as -6.64457584006e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.45685117514e-12.
Allowing negative dual variable(s) as small as -2.4004082752e-12.
Allowing negative dual variable(s) as small as -7.67767478698e-11.
Allowing negative dual variable(s) as small as -8.54843495689e-11.
Solving took 4 GP solves and 1.64 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93834314119e-12.
Allowing negative dual variable(s) as small as -3.89277473103e-11.
Allowing negative dual variable(s) as small as -5.41168030527e-11.
Allowing negative dual variable(s) as small as -5.45077355647e-11.
Solving took 4 GP solves and 2.05 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error