Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428145713)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.057065877167588e-14.
Allowing negative dual variable(s) as small as -7.563394355258879e-14.
Allowing negative dual variable(s) as small as -1.5110048628974582e-13.
Allowing negative dual variable(s) as small as -1.5022141516829457e-13.
Solving took 4 GP solves and 9.21 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.236219444149093e-14.
Allowing negative dual variable(s) as small as -7.451331218710777e-14.
Allowing negative dual variable(s) as small as -1.50637748802529e-13.
Allowing negative dual variable(s) as small as -1.4962293556908257e-13.
Solving took 4 GP solves and 5.2 seconds.
Allowing negative dual variable(s) as small as -5.173327044527554e-13.
Allowing negative dual variable(s) as small as -1.430536245017322e-12.
Allowing negative dual variable(s) as small as -4.449357549063393e-13.
Allowing negative dual variable(s) as small as -4.449895313340946e-13.
Allowing negative dual variable(s) as small as -1.298180530087678e-12.
Allowing negative dual variable(s) as small as -1.0910113958095824e-12.
Allowing negative dual variable(s) as small as -1.0914000822884184e-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
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 -2.54065856462483e-14.
Allowing negative dual variable(s) as small as -5.696073675709152e-12.
Allowing negative dual variable(s) as small as -2.0878964510413173e-11.
Allowing negative dual variable(s) as small as -2.0880853369321595e-11.
Solving took 4 GP solves and 3.75 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 6.93 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
Allowing negative dual variable(s) as small as -5.169788208636561e-13.
Allowing negative dual variable(s) as small as -1.4299880723989133e-12.
Allowing negative dual variable(s) as small as -4.44208905769905e-13.
Allowing negative dual variable(s) as small as -4.4462697412761543e-13.
Allowing negative dual variable(s) as small as -1.2970511166846e-12.
Allowing negative dual variable(s) as small as -1.0914550513385635e-12.
Allowing negative dual variable(s) as small as -1.0914336925557655e-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
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 -2.5046884740746408e-14.
Allowing negative dual variable(s) as small as -5.696090650937629e-12.
Allowing negative dual variable(s) as small as -2.0878972809059655e-11.
Allowing negative dual variable(s) as small as -2.0880856852215195e-11.
Solving took 4 GP solves and 6.92 seconds.
Max Speed [m/s]: 74.76
Beginning signomial solve.
Solving took 4 GP solves and 4.02 seconds.
Max payload weight [lbf] = 28.083
Max take off weight [lbf] = 166.417
	

Standard Error