Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171017121753)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.47111312988e-14.
Allowing negative dual variable(s) as small as -1.21423314112e-12.
Allowing negative dual variable(s) as small as -1.13634102128e-12.
Allowing negative dual variable(s) as small as -1.15124880115e-12.
Solving took 4 GP solves and 1.95 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.90466389461e-14.
Allowing negative dual variable(s) as small as -1.18703658014e-12.
Allowing negative dual variable(s) as small as -1.13059648449e-12.
Allowing negative dual variable(s) as small as -1.15178569807e-12.
Solving took 4 GP solves and 1.68 seconds.
Allowing negative dual variable(s) as small as -1.56981979499e-12.
Allowing negative dual variable(s) as small as -3.96074579384e-12.
Allowing negative dual variable(s) as small as -1.78671053647e-12.
Allowing negative dual variable(s) as small as -2.08185638867e-12.
Allowing negative dual variable(s) as small as -2.08109744715e-12.
Allowing negative dual variable(s) as small as -4.80314139156e-13.
Allowing negative dual variable(s) as small as -8.94229677285e-13.
Allowing negative dual variable(s) as small as -9.41481267946e-13.
Allowing negative dual variable(s) as small as -9.43160155011e-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 -2.38838462896e-13.
Allowing negative dual variable(s) as small as -9.26242589572e-14.
Allowing negative dual variable(s) as small as -1.20164186761e-13.
Allowing negative dual variable(s) as small as -1.20525442925e-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 -9.61917441706e-13.
Allowing negative dual variable(s) as small as -2.01716711077e-12.
Allowing negative dual variable(s) as small as -1.27541982327e-14.
Allowing negative dual variable(s) as small as -1.71969090698e-14.
Solving took 4 GP solves and 2.46 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 1.91 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56943815582e-12.
Allowing negative dual variable(s) as small as -3.96109967743e-12.
Allowing negative dual variable(s) as small as -1.78644338905e-12.
Allowing negative dual variable(s) as small as -2.08268818858e-12.
Allowing negative dual variable(s) as small as -2.08066897045e-12.
Allowing negative dual variable(s) as small as -4.74114454294e-13.
Allowing negative dual variable(s) as small as -8.93198167339e-13.
Allowing negative dual variable(s) as small as -9.419073594e-13.
Allowing negative dual variable(s) as small as -9.43064528379e-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 -2.3170397892e-13.
Allowing negative dual variable(s) as small as -9.2364158856e-14.
Allowing negative dual variable(s) as small as -1.19361226632e-13.
Allowing negative dual variable(s) as small as -1.20466570747e-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 -9.61297649064e-13.
Allowing negative dual variable(s) as small as -2.01675253237e-12.
Allowing negative dual variable(s) as small as -1.27118212802e-14.
Allowing negative dual variable(s) as small as -1.66097144376e-14.
Solving took 4 GP solves and 2.38 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 1.68 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error