Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180418162650)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.207670654236665e-14.
Allowing negative dual variable(s) as small as -8.188935640696116e-14.
Allowing negative dual variable(s) as small as -1.524097688332393e-13.
Allowing negative dual variable(s) as small as -1.5012600537711585e-13.
Solving took 4 GP solves and 2.08 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -7.939829349545846e-14.
Allowing negative dual variable(s) as small as -8.09807949864183e-14.
Allowing negative dual variable(s) as small as -1.5093438651692104e-13.
Allowing negative dual variable(s) as small as -1.500917445884653e-13.
Solving took 4 GP solves and 2.13 seconds.
Allowing negative dual variable(s) as small as -5.23197804525033e-13.
Allowing negative dual variable(s) as small as -5.141859160673334e-13.
Allowing negative dual variable(s) as small as -5.130357944027608e-13.
Allowing negative dual variable(s) as small as -5.157332894079047e-13.
Allowing negative dual variable(s) as small as -2.3984156674594637e-13.
Allowing negative dual variable(s) as small as -1.8391321451871612e-14.
Allowing negative dual variable(s) as small as -1.2592575636752312e-12.
Allowing negative dual variable(s) as small as -1.2592448785098131e-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 -1.588356182691264e-14.
Allowing negative dual variable(s) as small as -1.133602760272634e-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 -5.434121819968534e-11.
Allowing negative dual variable(s) as small as -6.449526823967958e-12.
Allowing negative dual variable(s) as small as -1.933927654586184e-11.
Allowing negative dual variable(s) as small as -1.9354577237980317e-11.
Solving took 4 GP solves and 1.89 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.43 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.226652444179081e-13.
Allowing negative dual variable(s) as small as -5.107650413727072e-13.
Allowing negative dual variable(s) as small as -5.175044420768771e-13.
Allowing negative dual variable(s) as small as -5.131103875122278e-13.
Allowing negative dual variable(s) as small as -2.3814674190991703e-13.
Allowing negative dual variable(s) as small as -1.8455180959831008e-14.
Allowing negative dual variable(s) as small as -1.2588036082256115e-12.
Allowing negative dual variable(s) as small as -1.2610094175455333e-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 -1.6986412276764895e-14.
Allowing negative dual variable(s) as small as -1.1471032457244235e-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 -5.4341232006534136e-11.
Allowing negative dual variable(s) as small as -6.449675653983068e-12.
Allowing negative dual variable(s) as small as -1.933919207356888e-11.
Allowing negative dual variable(s) as small as -1.935455715805845e-11.
Solving took 4 GP solves and 1.95 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 1.87 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error