Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171205104613)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.91819821117e-13.
Allowing negative dual variable(s) as small as -4.94759832062e-13.
Allowing negative dual variable(s) as small as -1.34026687318e-12.
Allowing negative dual variable(s) as small as -1.35732267439e-12.
Solving took 4 GP solves and 4.88 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.03807975042e-13.
Allowing negative dual variable(s) as small as -6.44699354665e-13.
Allowing negative dual variable(s) as small as -1.17824673629e-12.
Allowing negative dual variable(s) as small as -1.13646743925e-12.
Solving took 4 GP solves and 8.61 seconds.
Allowing negative dual variable(s) as small as -9.54648686491e-14.
Allowing negative dual variable(s) as small as -7.33067361154e-13.
Allowing negative dual variable(s) as small as -7.31781497378e-13.
Allowing negative dual variable(s) as small as -5.95630999031e-10.
Allowing negative dual variable(s) as small as -4.83015293344e-13.
Allowing negative dual variable(s) as small as -3.70078859051e-14.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -2.358063831e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.88431333242e-12.
Allowing negative dual variable(s) as small as -2.87606582975e-12.
Allowing negative dual variable(s) as small as -4.72567622419e-12.
Allowing negative dual variable(s) as small as -4.72774269559e-12.
Solving took 4 GP solves and 46.3 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 29.3 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
Allowing negative dual variable(s) as small as -9.62846339117e-14.
Allowing negative dual variable(s) as small as -7.34551850769e-13.
Allowing negative dual variable(s) as small as -7.33885608534e-13.
Allowing negative dual variable(s) as small as -5.95630344363e-10.
Allowing negative dual variable(s) as small as -4.84961842819e-13.
Allowing negative dual variable(s) as small as -3.58775780352e-14.
MTOW [lbs] = 132.53
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 = 20.352
speed at top of climb [m/s] = 25.000
design loiter speed [m/s] = 25.000
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 27.301
Allowing negative dual variable(s) as small as -2.11687492622e-14.
optimum loiter speed for min power, start of loiter [m/s] = 23.618
optimum loiter speed for min power, end of loiter [m/s] = 16.685
optimum cruise speed, inbound [m/s] = 31.024
optimum cruise speed, outbound [m/s] = 23.411
Beginning signomial solve.
Allowing negative dual variable(s) as small as -8.88445930509e-12.
Allowing negative dual variable(s) as small as -2.8760482487e-12.
Allowing negative dual variable(s) as small as -4.72558463793e-12.
Allowing negative dual variable(s) as small as -4.72775367157e-12.
Solving took 4 GP solves and 5.19 seconds.
Max Speed [m/s]: 64.61
Beginning signomial solve.
Solving took 4 GP solves and 9.31 seconds.
Max payload weight [lbf] = 9.228
Max take off weight [lbf] = 140.364
	

Standard Error