Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171120111847)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.01064122349e-13.
Allowing negative dual variable(s) as small as -1.98030957951e-12.
Allowing negative dual variable(s) as small as -2.16813459547e-12.
Allowing negative dual variable(s) as small as -2.16217451929e-12.
Solving took 4 GP solves and 3.15 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.03880012231e-13.
Allowing negative dual variable(s) as small as -1.91096184016e-12.
Allowing negative dual variable(s) as small as -2.16344260215e-12.
Allowing negative dual variable(s) as small as -2.1612403707e-12.
Solving took 4 GP solves and 2.79 seconds.
Allowing negative dual variable(s) as small as -1.21215537607e-13.
Allowing negative dual variable(s) as small as -8.16039943952e-14.
Allowing negative dual variable(s) as small as -2.06891795362e-14.
Allowing negative dual variable(s) as small as -2.06709649397e-14.
Allowing negative dual variable(s) as small as -1.04198680934e-12.
Allowing negative dual variable(s) as small as -1.64569790087e-12.
Allowing negative dual variable(s) as small as -1.46588362109e-12.
Allowing negative dual variable(s) as small as -1.46663692475e-12.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12616816914e-12.
Allowing negative dual variable(s) as small as -1.65453501594e-12.
Allowing negative dual variable(s) as small as -1.63622696121e-12.
Allowing negative dual variable(s) as small as -1.63905933097e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25444859476e-11.
Allowing negative dual variable(s) as small as -4.86405550341e-11.
Allowing negative dual variable(s) as small as -4.1382004634e-12.
Allowing negative dual variable(s) as small as -4.13946265562e-12.
Solving took 4 GP solves and 2.49 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.67 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -1.21304875866e-13.
Allowing negative dual variable(s) as small as -8.15103193275e-14.
Allowing negative dual variable(s) as small as -2.05720857016e-14.
Allowing negative dual variable(s) as small as -2.07819872422e-14.
Allowing negative dual variable(s) as small as -1.04149024474e-12.
Allowing negative dual variable(s) as small as -1.64480061515e-12.
Allowing negative dual variable(s) as small as -1.46575395051e-12.
Allowing negative dual variable(s) as small as -1.46436508752e-12.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -1.12415697411e-12.
Allowing negative dual variable(s) as small as -1.65719716595e-12.
Allowing negative dual variable(s) as small as -1.63675865396e-12.
Allowing negative dual variable(s) as small as -1.63792829126e-12.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.25445371401e-11.
Allowing negative dual variable(s) as small as -4.86406448458e-11.
Allowing negative dual variable(s) as small as -4.13824471786e-12.
Allowing negative dual variable(s) as small as -4.13935282428e-12.
Solving took 4 GP solves and 2.95 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 1.72 seconds.
Max payload weight [lbf] = 8.892
Max take off weight [lbf] = 140.364
	

Standard Error