Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018091628)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.00446560791e-13.
Allowing negative dual variable(s) as small as -1.18027592907e-12.
Allowing negative dual variable(s) as small as -1.13900252077e-12.
Allowing negative dual variable(s) as small as -1.14319361269e-12.
Solving took 4 GP solves and 26.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.43255890062e-14.
Allowing negative dual variable(s) as small as -1.2093824206e-12.
Allowing negative dual variable(s) as small as -1.15707573731e-12.
Allowing negative dual variable(s) as small as -1.13543939875e-12.
Solving took 4 GP solves and 28.6 seconds.
Allowing negative dual variable(s) as small as -1.56939131829e-12.
Allowing negative dual variable(s) as small as -3.96085247933e-12.
Allowing negative dual variable(s) as small as -1.78658303429e-12.
Allowing negative dual variable(s) as small as -2.08263527951e-12.
Allowing negative dual variable(s) as small as -2.08009044017e-12.
Allowing negative dual variable(s) as small as -4.73210012841e-13.
Allowing negative dual variable(s) as small as -8.93342040967e-13.
Allowing negative dual variable(s) as small as -9.4240110507e-13.
Allowing negative dual variable(s) as small as -9.42154557496e-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 -2.31707231527e-13.
Allowing negative dual variable(s) as small as -9.23395474667e-14.
Allowing negative dual variable(s) as small as -1.20226094705e-13.
Allowing negative dual variable(s) as small as -1.21273108743e-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 -9.61265165562e-13.
Allowing negative dual variable(s) as small as -2.01714821947e-12.
Allowing negative dual variable(s) as small as -1.28324574596e-14.
Allowing negative dual variable(s) as small as -1.79674748472e-14.
Solving took 4 GP solves and 2.43 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 4.76 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56954050451e-12.
Allowing negative dual variable(s) as small as -3.96060875069e-12.
Allowing negative dual variable(s) as small as -1.78671227119e-12.
Allowing negative dual variable(s) as small as -2.08251731831e-12.
Allowing negative dual variable(s) as small as -2.08076698233e-12.
Allowing negative dual variable(s) as small as -4.71169110672e-13.
Allowing negative dual variable(s) as small as -8.92677099774e-13.
Allowing negative dual variable(s) as small as -9.41750150085e-13.
Allowing negative dual variable(s) as small as -9.43759501972e-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 -2.34481921726e-13.
Allowing negative dual variable(s) as small as -9.24486182052e-14.
Allowing negative dual variable(s) as small as -1.19091260291e-13.
Allowing negative dual variable(s) as small as -1.2066790709e-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 -9.60998432346e-13.
Allowing negative dual variable(s) as small as -2.01734477289e-12.
Allowing negative dual variable(s) as small as -1.31655362784e-14.
Allowing negative dual variable(s) as small as -1.68835747478e-14.
Solving took 4 GP solves and 2.45 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 5.22 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error