Skip to content

Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180418170939)

Took 1 min 27 sec.

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.049333768966882e-14.
Allowing negative dual variable(s) as small as -8.760873970725669e-14.
Allowing negative dual variable(s) as small as -1.5112954290796843e-13.
Allowing negative dual variable(s) as small as -1.5043044934714978e-13.
Solving took 4 GP solves and 64.5 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.317695490700494e-14.
Allowing negative dual variable(s) as small as -8.080732263882062e-14.
Allowing negative dual variable(s) as small as -1.4955831711960244e-13.
Allowing negative dual variable(s) as small as -1.5007916784326447e-13.
Solving took 4 GP solves and 22 seconds.
Allowing negative dual variable(s) as small as -5.222523802306256e-13.
Allowing negative dual variable(s) as small as -5.114832168917616e-13.
Allowing negative dual variable(s) as small as -5.141078535109145e-13.
Allowing negative dual variable(s) as small as -5.155962462533026e-13.
Allowing negative dual variable(s) as small as -2.376783665714033e-13.
Allowing negative dual variable(s) as small as -1.9582317538346938e-14.
Allowing negative dual variable(s) as small as -1.259869053700513e-12.
Allowing negative dual variable(s) as small as -1.2593457093118543e-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 -2.140431928920883e-14.
Allowing negative dual variable(s) as small as -1.134493974458417e-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 -5.4341229801389737e-11.
Allowing negative dual variable(s) as small as -6.449592230899233e-12.
Allowing negative dual variable(s) as small as -1.9339248700500732e-11.
Allowing negative dual variable(s) as small as -1.935462213326762e-11.
Solving took 4 GP solves and 19.8 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 22.2 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.227294291865192e-13.
Allowing negative dual variable(s) as small as -5.144617371000137e-13.
Allowing negative dual variable(s) as small as -5.154557336517485e-13.
Allowing negative dual variable(s) as small as -5.161131938491437e-13.
Allowing negative dual variable(s) as small as -2.3459793135893747e-13.
Allowing negative dual variable(s) as small as -1.9450044873303707e-14.
Allowing negative dual variable(s) as small as -1.2617973072642785e-12.
Allowing negative dual variable(s) as small as -1.2602544875728316e-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 -1.9030350212334568e-14.
Allowing negative dual variable(s) as small as -1.1482178055577386e-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 -5.434126197593624e-11.
Allowing negative dual variable(s) as small as -6.449628225299629e-12.
Allowing negative dual variable(s) as small as -1.933920462050911e-11.
Allowing negative dual variable(s) as small as -1.9354525357476995e-11.
Solving took 4 GP solves and 21 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.65 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error