Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171017122017)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.5806175493e-14.
Allowing negative dual variable(s) as small as -1.19494605183e-12.
Allowing negative dual variable(s) as small as -1.14565128218e-12.
Allowing negative dual variable(s) as small as -1.13246434799e-12.
Solving took 4 GP solves and 4.57 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.0024620023e-13.
Allowing negative dual variable(s) as small as -1.19035987664e-12.
Allowing negative dual variable(s) as small as -1.12453405962e-12.
Allowing negative dual variable(s) as small as -1.13323586626e-12.
Solving took 4 GP solves and 7.17 seconds.
Allowing negative dual variable(s) as small as -1.56930544948e-12.
Allowing negative dual variable(s) as small as -3.96113870871e-12.
Allowing negative dual variable(s) as small as -1.78664461697e-12.
Allowing negative dual variable(s) as small as -2.08251124678e-12.
Allowing negative dual variable(s) as small as -2.08072534896e-12.
Allowing negative dual variable(s) as small as -4.79237092718e-13.
Allowing negative dual variable(s) as small as -8.92740091921e-13.
Allowing negative dual variable(s) as small as -9.40313148526e-13.
Allowing negative dual variable(s) as small as -9.43079490369e-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 -2.33709752939e-13.
Allowing negative dual variable(s) as small as -9.22994319863e-14.
Allowing negative dual variable(s) as small as -1.1938052543e-13.
Allowing negative dual variable(s) as small as -1.20048068708e-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 -9.61038613471e-13.
Allowing negative dual variable(s) as small as -2.01653468281e-12.
Allowing negative dual variable(s) as small as -1.28584513655e-14.
Allowing negative dual variable(s) as small as -1.75682598017e-14.
Solving took 4 GP solves and 3.6 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 4.14 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56944075791e-12.
Allowing negative dual variable(s) as small as -3.95979256329e-12.
Allowing negative dual variable(s) as small as -1.78678166013e-12.
Allowing negative dual variable(s) as small as -2.08223629311e-12.
Allowing negative dual variable(s) as small as -2.08082856501e-12.
Allowing negative dual variable(s) as small as -4.69576851361e-13.
Allowing negative dual variable(s) as small as -8.93376627016e-13.
Allowing negative dual variable(s) as small as -9.40989365421e-13.
Allowing negative dual variable(s) as small as -9.42797272543e-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 -2.35601902571e-13.
Allowing negative dual variable(s) as small as -9.29259924218e-14.
Allowing negative dual variable(s) as small as -1.20415830085e-13.
Allowing negative dual variable(s) as small as -1.20071812736e-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 -9.60981985295e-13.
Allowing negative dual variable(s) as small as -2.01709333994e-12.
Allowing negative dual variable(s) as small as -1.31524234143e-14.
Allowing negative dual variable(s) as small as -1.76877998146e-14.
Solving took 4 GP solves and 2.84 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 1.76 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error