Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171110164928)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.12312936729e-13.
Allowing negative dual variable(s) as small as -1.05036205428e-13.
Allowing negative dual variable(s) as small as -1.08853898118e-16.
Allowing negative dual variable(s) as small as -1.95156391047e-17.
Solving took 4 GP solves and 29.2 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.10144966065e-13.
Allowing negative dual variable(s) as small as -1.08233734475e-13.
Allowing negative dual variable(s) as small as -3.77302356025e-17.
Solving took 4 GP solves and 5.49 seconds.
Allowing negative dual variable(s) as small as -3.88189393824e-12.
Allowing negative dual variable(s) as small as -1.71229263407e-12.
Allowing negative dual variable(s) as small as -7.74707555051e-13.
Allowing negative dual variable(s) as small as -7.71005655154e-13.
Allowing negative dual variable(s) as small as -7.69818236934e-13.
Allowing negative dual variable(s) as small as -2.52605662082e-13.
Allowing negative dual variable(s) as small as -1.01679244451e-12.
Allowing negative dual variable(s) as small as -1.05939204891e-12.
Allowing negative dual variable(s) as small as -1.047310242e-12.
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 -2.57926709504e-13.
Allowing negative dual variable(s) as small as -1.47499525614e-13.
Allowing negative dual variable(s) as small as -1.48036639371e-13.
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 -4.00777321257e-13.
Allowing negative dual variable(s) as small as -1.08858816203e-15.
Allowing negative dual variable(s) as small as -9.02847071053e-14.
Allowing negative dual variable(s) as small as -8.94709980224e-14.
Solving took 4 GP solves and 3.27 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 1.29 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -3.88089560488e-12.
Allowing negative dual variable(s) as small as -1.7121764076e-12.
Allowing negative dual variable(s) as small as -7.75813441267e-13.
Allowing negative dual variable(s) as small as -7.70123548266e-13.
Allowing negative dual variable(s) as small as -7.70267530315e-13.
Allowing negative dual variable(s) as small as -2.49985579112e-13.
Allowing negative dual variable(s) as small as -1.01836594713e-12.
Allowing negative dual variable(s) as small as -1.05841388171e-12.
Allowing negative dual variable(s) as small as -1.0473606574e-12.
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 -2.58686084706e-13.
Allowing negative dual variable(s) as small as -1.49176461114e-13.
Allowing negative dual variable(s) as small as -1.48458068755e-13.
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 -4.00344800823e-13.
Allowing negative dual variable(s) as small as -1.97717289284e-15.
Allowing negative dual variable(s) as small as -8.88830193024e-14.
Allowing negative dual variable(s) as small as -8.81235854967e-14.
Solving took 4 GP solves and 27.8 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Solving took 4 GP solves and 4.85 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error