Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180418151545)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.944946783799978e-14.
Allowing negative dual variable(s) as small as -7.757249703699287e-14.
Allowing negative dual variable(s) as small as -1.5140666498325572e-13.
Allowing negative dual variable(s) as small as -1.4888958121961338e-13.
Solving took 4 GP solves and 2.63 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.975087604195075e-14.
Allowing negative dual variable(s) as small as -7.989008760089789e-14.
Allowing negative dual variable(s) as small as -1.523351757237723e-13.
Allowing negative dual variable(s) as small as -1.4917624427401854e-13.
Solving took 4 GP solves and 2.85 seconds.
Allowing negative dual variable(s) as small as -5.269291947218591e-13.
Allowing negative dual variable(s) as small as -5.1309650972442e-13.
Allowing negative dual variable(s) as small as -5.153828752657574e-13.
Allowing negative dual variable(s) as small as -5.143264286688876e-13.
Allowing negative dual variable(s) as small as -2.337964891130362e-13.
Allowing negative dual variable(s) as small as -1.7273509012039057e-14.
Allowing negative dual variable(s) as small as -1.2593064611932103e-12.
Allowing negative dual variable(s) as small as -1.2589834773660269e-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 -1.822847428556429e-14.
Allowing negative dual variable(s) as small as -1.1268611911641191e-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 -5.4341249703487624e-11.
Allowing negative dual variable(s) as small as -6.4495933586971326e-12.
Allowing negative dual variable(s) as small as -1.9339280565880208e-11.
Allowing negative dual variable(s) as small as -1.9354581201565114e-11.
Solving took 4 GP solves and 3.07 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.44 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.246827278204691e-13.
Allowing negative dual variable(s) as small as -5.114346446344342e-13.
Allowing negative dual variable(s) as small as -5.150012361010425e-13.
Allowing negative dual variable(s) as small as -5.134764141656589e-13.
Allowing negative dual variable(s) as small as -2.39345002150948e-13.
Allowing negative dual variable(s) as small as -1.8699885390160986e-14.
Allowing negative dual variable(s) as small as -1.2610626518722023e-12.
Allowing negative dual variable(s) as small as -1.2601552830740492e-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 -2.1201790323388536e-14.
Allowing negative dual variable(s) as small as -1.1425279125565346e-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 -5.434134748158292e-11.
Allowing negative dual variable(s) as small as -6.449625752863395e-12.
Allowing negative dual variable(s) as small as -1.933921664144188e-11.
Allowing negative dual variable(s) as small as -1.9354600183149946e-11.
Solving took 4 GP solves and 1.73 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.32 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error