Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171101154537)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.78808616419e-12.
Allowing negative dual variable(s) as small as -1.85350745169e-11.
Allowing negative dual variable(s) as small as -4.41732588008e-13.
Allowing negative dual variable(s) as small as -4.41112424365e-13.
Solving took 4 GP solves and 1.6 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.8538261124e-12.
Allowing negative dual variable(s) as small as -9.60799061839e-12.
Allowing negative dual variable(s) as small as -4.80638966127e-13.
Allowing negative dual variable(s) as small as -4.32150842888e-13.
Solving took 4 GP solves and 2.61 seconds.
Allowing negative dual variable(s) as small as -2.31723321087e-11.
Allowing negative dual variable(s) as small as -8.76654304705e-12.
Allowing negative dual variable(s) as small as -1.9860356415e-11.
Allowing negative dual variable(s) as small as -7.67659547041e-12.
Allowing negative dual variable(s) as small as -7.67528401946e-12.
Allowing negative dual variable(s) as small as -2.36051172098e-11.
Allowing negative dual variable(s) as small as -1.1789909435e-11.
Allowing negative dual variable(s) as small as -1.19803968178e-11.
Allowing negative dual variable(s) as small as -1.17689118e-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 -2.73304686174e-11.
Allowing negative dual variable(s) as small as -1.24169707719e-11.
Allowing negative dual variable(s) as small as -7.11382211818e-12.
Allowing negative dual variable(s) as small as -6.6468787939e-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 -1.45660715087e-12.
Allowing negative dual variable(s) as small as -2.40161769362e-12.
Allowing negative dual variable(s) as small as -7.67824206946e-11.
Allowing negative dual variable(s) as small as -8.54864584378e-11.
Solving took 4 GP solves and 1.96 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93497040507e-12.
Allowing negative dual variable(s) as small as -3.89196183961e-11.
Allowing negative dual variable(s) as small as -5.40948982657e-11.
Allowing negative dual variable(s) as small as -5.45092382689e-11.
Solving took 4 GP solves and 1.39 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.31165295239e-11.
Allowing negative dual variable(s) as small as -8.77221212336e-12.
Allowing negative dual variable(s) as small as -1.99141675372e-11.
Allowing negative dual variable(s) as small as -7.69053570826e-12.
Allowing negative dual variable(s) as small as -7.7196304904e-12.
Allowing negative dual variable(s) as small as -2.3609199231e-11.
Allowing negative dual variable(s) as small as -1.17842516344e-11.
Allowing negative dual variable(s) as small as -1.1977771856e-11.
Allowing negative dual variable(s) as small as -1.17664502274e-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 -2.73228549161e-11.
Allowing negative dual variable(s) as small as -1.24212393843e-11.
Allowing negative dual variable(s) as small as -7.11320455662e-12.
Allowing negative dual variable(s) as small as -6.64687705917e-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 -1.45672126485e-12.
Allowing negative dual variable(s) as small as -2.40074482002e-12.
Allowing negative dual variable(s) as small as -7.67880404618e-11.
Allowing negative dual variable(s) as small as -8.54816274972e-11.
Solving took 4 GP solves and 1.72 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93158205644e-12.
Allowing negative dual variable(s) as small as -3.89198642932e-11.
Allowing negative dual variable(s) as small as -5.40947668604e-11.
Allowing negative dual variable(s) as small as -5.45025491752e-11.
Solving took 4 GP solves and 1.54 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error