Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180124112533)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.8488292494178715e-13.
Allowing negative dual variable(s) as small as -9.297337205671496e-14.
Allowing negative dual variable(s) as small as -5.763532012759143e-14.
Allowing negative dual variable(s) as small as -5.369793151799307e-14.
Solving took 4 GP solves and 3.88 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.7598162510568116e-13.
Allowing negative dual variable(s) as small as -9.124688851724905e-14.
Allowing negative dual variable(s) as small as -5.6025930422753945e-14.
Allowing negative dual variable(s) as small as -5.5172446472573355e-14.
Solving took 4 GP solves and 3.29 seconds.
Allowing negative dual variable(s) as small as -5.975237665767352e-13.
Allowing negative dual variable(s) as small as -1.4369911510714317e-12.
Allowing negative dual variable(s) as small as -1.6874834862790067e-12.
Allowing negative dual variable(s) as small as -1.6870992450290778e-12.
Allowing negative dual variable(s) as small as -1.3467805429906443e-12.
Allowing negative dual variable(s) as small as -2.2114172472387228e-12.
Allowing negative dual variable(s) as small as -2.280291840767168e-13.
Allowing negative dual variable(s) as small as -2.276844077858664e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.7867053322961901e-12.
Allowing negative dual variable(s) as small as -2.0149485378817555e-13.
Allowing negative dual variable(s) as small as -2.2896745263678575e-13.
Allowing negative dual variable(s) as small as -2.236082412981899e-13.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.2877365188001584e-11.
Allowing negative dual variable(s) as small as -8.751066684399549e-12.
Allowing negative dual variable(s) as small as -8.175280844628262e-12.
Allowing negative dual variable(s) as small as -8.174480486885627e-12.
Solving took 4 GP solves and 47.7 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Solving took 4 GP solves and 1.28 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
Allowing negative dual variable(s) as small as -5.974890721072157e-13.
Allowing negative dual variable(s) as small as -1.4370310497113792e-12.
Allowing negative dual variable(s) as small as -1.6874097605312777e-12.
Allowing negative dual variable(s) as small as -1.687006437323113e-12.
Allowing negative dual variable(s) as small as -1.3522789658881873e-12.
Allowing negative dual variable(s) as small as -2.2105041321690555e-12.
Allowing negative dual variable(s) as small as -2.296756534958533e-13.
Allowing negative dual variable(s) as small as -2.326654494066993e-13.
MTOW [lbs] = 134.67
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 = 20.615
speed at top of climb [m/s] = 25.153
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.521
Allowing negative dual variable(s) as small as -1.7915478128793794e-12.
Allowing negative dual variable(s) as small as -2.0086623336856846e-13.
Allowing negative dual variable(s) as small as -2.2565586552114603e-13.
Allowing negative dual variable(s) as small as -2.2330054472163852e-13.
optimum loiter speed for min power, start of loiter [m/s] = 23.910
optimum loiter speed for min power, end of loiter [m/s] = 16.760
optimum cruise speed, inbound [m/s] = 31.821
optimum cruise speed, outbound [m/s] = 23.768
Beginning signomial solve.
Allowing negative dual variable(s) as small as -2.287751788570148e-11.
Allowing negative dual variable(s) as small as -8.751183986005404e-12.
Allowing negative dual variable(s) as small as -8.17540795406501e-12.
Allowing negative dual variable(s) as small as -8.174390694153734e-12.
Solving took 4 GP solves and 4.15 seconds.
Max Speed [m/s]: 66.56
Beginning signomial solve.
Solving took 4 GP solves and 1.5 seconds.
Max payload weight [lbf] = 12.624
Max take off weight [lbf] = 145.409
	

Standard Error