Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171031145109)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.84471360998e-12.
Allowing negative dual variable(s) as small as -1.84747811667e-11.
Allowing negative dual variable(s) as small as -3.96144055059e-13.
Allowing negative dual variable(s) as small as -4.94043174426e-13.
Solving took 4 GP solves and 6.21 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.79256478653e-12.
Allowing negative dual variable(s) as small as -9.67496612339e-12.
Allowing negative dual variable(s) as small as -3.52153202432e-13.
Allowing negative dual variable(s) as small as -8.41817934805e-15.
Solving took 4 GP solves and 4.94 seconds.
Allowing negative dual variable(s) as small as -2.31432581432e-11.
Allowing negative dual variable(s) as small as -8.79097489248e-12.
Allowing negative dual variable(s) as small as -1.98819016806e-11.
Allowing negative dual variable(s) as small as -7.66482016745e-12.
Allowing negative dual variable(s) as small as -7.70269265038e-12.
Allowing negative dual variable(s) as small as -2.36070908915e-11.
Allowing negative dual variable(s) as small as -1.1785547256e-11.
Allowing negative dual variable(s) as small as -1.19785358932e-11.
Allowing negative dual variable(s) as small as -1.17712208253e-11.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.73276735442e-11.
Allowing negative dual variable(s) as small as -1.24187425751e-11.
Allowing negative dual variable(s) as small as -7.11076206597e-12.
Allowing negative dual variable(s) as small as -6.64489828179e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.45710440495e-12.
Allowing negative dual variable(s) as small as -2.39970666786e-12.
Allowing negative dual variable(s) as small as -7.67885649465e-11.
Allowing negative dual variable(s) as small as -8.5480269768e-11.
Solving took 4 GP solves and 14 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.9350831621e-12.
Allowing negative dual variable(s) as small as -3.89178186205e-11.
Allowing negative dual variable(s) as small as -5.41035020604e-11.
Allowing negative dual variable(s) as small as -5.45069393267e-11.
Solving took 4 GP solves and 1.43 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
Allowing negative dual variable(s) as small as -2.31928920513e-11.
Allowing negative dual variable(s) as small as -8.81361650329e-12.
Allowing negative dual variable(s) as small as -1.99390295941e-11.
Allowing negative dual variable(s) as small as -7.6759154588e-12.
Allowing negative dual variable(s) as small as -7.68732993928e-12.
Allowing negative dual variable(s) as small as -2.36110488799e-11.
Allowing negative dual variable(s) as small as -1.1785149137e-11.
Allowing negative dual variable(s) as small as -1.19773824105e-11.
Allowing negative dual variable(s) as small as -1.17719168831e-11.
MTOW [lbs] = 141.59
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 = 21.754
speed at top of climb [m/s] = 26.532
design loiter speed [m/s] = 25.052
rotation speed at 55 lbs [m/s] = 18.158
rotation speed at 150 lbs [m/s] = 28.219
Allowing negative dual variable(s) as small as -2.73232573719e-11.
Allowing negative dual variable(s) as small as -1.24222134315e-11.
Allowing negative dual variable(s) as small as -7.11219527282e-12.
Allowing negative dual variable(s) as small as -6.64838128127e-12.
optimum loiter speed for min power, start of loiter [m/s] = 25.190
optimum loiter speed for min power, end of loiter [m/s] = 17.170
optimum cruise speed, inbound [m/s] = 35.882
optimum cruise speed, outbound [m/s] = 25.488
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.45698231447e-12.
Allowing negative dual variable(s) as small as -2.40041289576e-12.
Allowing negative dual variable(s) as small as -7.67867551983e-11.
Allowing negative dual variable(s) as small as -8.54773548038e-11.
Solving took 4 GP solves and 2.08 seconds.
Max Speed [m/s]: 74.36
Beginning signomial solve.
Allowing negative dual variable(s) as small as -3.95510187101e-12.
Allowing negative dual variable(s) as small as -3.89330919934e-11.
Allowing negative dual variable(s) as small as -5.41059939907e-11.
Allowing negative dual variable(s) as small as -5.45221246623e-11.
Solving took 4 GP solves and 1.37 seconds.
Max payload weight [lbf] = 27.204
Max take off weight [lbf] = 165.012
	

Standard Error