Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018110828)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.6451492626e-14.
Allowing negative dual variable(s) as small as -1.1903178096e-12.
Allowing negative dual variable(s) as small as -1.13790660922e-12.
Allowing negative dual variable(s) as small as -1.13608558325e-12.
Solving took 4 GP solves and 27.4 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.42058930864e-14.
Allowing negative dual variable(s) as small as -1.1918842649e-12.
Allowing negative dual variable(s) as small as -1.15241236692e-12.
Allowing negative dual variable(s) as small as -1.14765575515e-12.
Solving took 4 GP solves and 30.4 seconds.
Allowing negative dual variable(s) as small as -1.56932713352e-12.
Allowing negative dual variable(s) as small as -3.96075446746e-12.
Allowing negative dual variable(s) as small as -1.78743478352e-12.
Allowing negative dual variable(s) as small as -2.08265869828e-12.
Allowing negative dual variable(s) as small as -2.0810714263e-12.
Allowing negative dual variable(s) as small as -4.69092429831e-13.
Allowing negative dual variable(s) as small as -8.91690692638e-13.
Allowing negative dual variable(s) as small as -9.41326769137e-13.
Allowing negative dual variable(s) as small as -9.42388636745e-13.
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
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 -2.27294528685e-13.
Allowing negative dual variable(s) as small as -9.21385363839e-14.
Allowing negative dual variable(s) as small as -1.21044884185e-13.
Allowing negative dual variable(s) as small as -1.21578528495e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61294109313e-13.
Allowing negative dual variable(s) as small as -2.016644311e-12.
Allowing negative dual variable(s) as small as -1.32683605725e-14.
Allowing negative dual variable(s) as small as -1.7050543947e-14.
Solving took 4 GP solves and 7.23 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 16.1 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56958560732e-12.
Allowing negative dual variable(s) as small as -3.96093921551e-12.
Allowing negative dual variable(s) as small as -1.78641389875e-12.
Allowing negative dual variable(s) as small as -2.08245400091e-12.
Allowing negative dual variable(s) as small as -2.08044605848e-12.
Allowing negative dual variable(s) as small as -4.72975608332e-13.
Allowing negative dual variable(s) as small as -8.94017932601e-13.
Allowing negative dual variable(s) as small as -9.41570389365e-13.
Allowing negative dual variable(s) as small as -9.42493587515e-13.
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 = 21.712
speed at top of climb [m/s] = 26.507
design loiter speed [m/s] = 25.048
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 -2.36618884208e-13.
Allowing negative dual variable(s) as small as -9.12046046325e-14.
Allowing negative dual variable(s) as small as -1.19826999885e-13.
Allowing negative dual variable(s) as small as -1.20144779542e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.166
optimum loiter speed for min power, end of loiter [m/s] = 17.158
optimum cruise speed, inbound [m/s] = 35.697
optimum cruise speed, outbound [m/s] = 25.443
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.61220657157e-13.
Allowing negative dual variable(s) as small as -2.01615843564e-12.
Allowing negative dual variable(s) as small as -1.33570264461e-14.
Allowing negative dual variable(s) as small as -1.71804923007e-14.
Solving took 4 GP solves and 26.4 seconds.
Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000
Max Speed [m/s]: 73.83
Beginning signomial solve.
Solving took 4 GP solves and 3.26 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error