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Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180402123416)

Took 5.2 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.925691353216635e-14.
Allowing negative dual variable(s) as small as -8.140146542934268e-14.
Allowing negative dual variable(s) as small as -1.5041266843152101e-13.
Allowing negative dual variable(s) as small as -1.4960862410040576e-13.
Solving took 4 GP solves and 2.98 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.081122576664157e-14.
Allowing negative dual variable(s) as small as -8.003493701114195e-14.
Allowing negative dual variable(s) as small as -1.5264352282162719e-13.
Allowing negative dual variable(s) as small as -1.482525040230609e-13.
Solving took 4 GP solves and 2.96 seconds.
Allowing negative dual variable(s) as small as -5.239038369797555e-13.
Allowing negative dual variable(s) as small as -5.109385137203049e-13.
Allowing negative dual variable(s) as small as -5.152475668346312e-13.
Allowing negative dual variable(s) as small as -5.14146017427386e-13.
Allowing negative dual variable(s) as small as -2.3555636607941466e-13.
Allowing negative dual variable(s) as small as -1.8792584675908497e-14.
Allowing negative dual variable(s) as small as -1.2597645366110855e-12.
Allowing negative dual variable(s) as small as -1.2597995563412567e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -1.9730744815760204e-14.
Allowing negative dual variable(s) as small as -1.1378506643844322e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.4341283028728384e-11.
Allowing negative dual variable(s) as small as -6.4495327605836575e-12.
Allowing negative dual variable(s) as small as -1.933934127230802e-11.
Allowing negative dual variable(s) as small as -1.935451975305703e-11.
Solving took 4 GP solves and 2.9 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.92 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.23494442239425e-13.
Allowing negative dual variable(s) as small as -5.114970946795694e-13.
Allowing negative dual variable(s) as small as -5.173847461570347e-13.
Allowing negative dual variable(s) as small as -5.157766574948042e-13.
Allowing negative dual variable(s) as small as -2.360004552892647e-13.
Allowing negative dual variable(s) as small as -1.9179970112137568e-14.
Allowing negative dual variable(s) as small as -1.2596335649886492e-12.
Allowing negative dual variable(s) as small as -1.2610534361537362e-12.
MTOW [lbs] = 141.77
Zero fuel weight [lbs] = 53.80
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 = 21.829
speed at top of climb [m/s] = 26.622
design loiter speed [m/s] = 25.070
rotation speed at 55 lbs [m/s] = 18.185
rotation speed at 150 lbs [m/s] = 28.236
Allowing negative dual variable(s) as small as -2.2930442267199425e-14.
Allowing negative dual variable(s) as small as -1.138240977166527e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.279
optimum loiter speed for min power, end of loiter [m/s] = 17.233
optimum cruise speed, inbound [m/s] = 36.269
optimum cruise speed, outbound [m/s] = 25.637
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.434124419724407e-11.
Allowing negative dual variable(s) as small as -6.449742085400693e-12.
Allowing negative dual variable(s) as small as -1.9339098099604428e-11.
Allowing negative dual variable(s) as small as -1.9354551708724924e-11.
Solving took 4 GP solves and 2.97 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.74 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error