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Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171031162735)

Took 7.9 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.77472835975e-12.
Allowing negative dual variable(s) as small as -9.61490782825e-12.
Allowing negative dual variable(s) as small as -3.26062527672e-13.
Allowing negative dual variable(s) as small as -4.54807198846e-13.
Solving took 4 GP solves and 1.51 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.77291687476e-12.
Allowing negative dual variable(s) as small as -9.92550442877e-12.
Allowing negative dual variable(s) as small as -3.62745857657e-13.
Allowing negative dual variable(s) as small as -3.97383514983e-13.
Solving took 4 GP solves and 1.58 seconds.
Allowing negative dual variable(s) as small as -2.3163547469e-11.
Allowing negative dual variable(s) as small as -8.80943928916e-12.
Allowing negative dual variable(s) as small as -1.98808747243e-11.
Allowing negative dual variable(s) as small as -7.66094826465e-12.
Allowing negative dual variable(s) as small as -7.67107904975e-12.
Allowing negative dual variable(s) as small as -2.36052774549e-11.
Allowing negative dual variable(s) as small as -1.178475156e-11.
Allowing negative dual variable(s) as small as -1.1977426646e-11.
Allowing negative dual variable(s) as small as -1.17692515889e-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 -2.73263607922e-11.
Allowing negative dual variable(s) as small as -1.24179423255e-11.
Allowing negative dual variable(s) as small as -7.11417838702e-12.
Allowing negative dual variable(s) as small as -6.64684648467e-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 -1.45700945341e-12.
Allowing negative dual variable(s) as small as -2.40017523166e-12.
Allowing negative dual variable(s) as small as -7.67860599243e-11.
Allowing negative dual variable(s) as small as -8.54822565327e-11.
Solving took 4 GP solves and 7.64 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.93054512549e-12.
Allowing negative dual variable(s) as small as -3.89311083371e-11.
Allowing negative dual variable(s) as small as -5.40953692431e-11.
Allowing negative dual variable(s) as small as -5.45062402331e-11.
Solving took 4 GP solves and 14.7 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.31494823311e-11.
Allowing negative dual variable(s) as small as -8.8004048493e-12.
Allowing negative dual variable(s) as small as -1.98649152683e-11.
Allowing negative dual variable(s) as small as -7.70204039435e-12.
Allowing negative dual variable(s) as small as -7.68641400528e-12.
Allowing negative dual variable(s) as small as -2.36071479205e-11.
Allowing negative dual variable(s) as small as -1.17863616002e-11.
Allowing negative dual variable(s) as small as -1.19808273545e-11.
Allowing negative dual variable(s) as small as -1.17703736298e-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 -2.73213120964e-11.
Allowing negative dual variable(s) as small as -1.24217355152e-11.
Allowing negative dual variable(s) as small as -7.11317593369e-12.
Allowing negative dual variable(s) as small as -6.64705378413e-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 -1.45675088305e-12.
Allowing negative dual variable(s) as small as -2.40009725423e-12.
Allowing negative dual variable(s) as small as -7.67886239631e-11.
Allowing negative dual variable(s) as small as -8.54848353039e-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 -3.94587921365e-12.
Allowing negative dual variable(s) as small as -3.89198716658e-11.
Allowing negative dual variable(s) as small as -5.40943088934e-11.
Allowing negative dual variable(s) as small as -5.45115328744e-11.
Solving took 4 GP solves and 1.48 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error