Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171011221930)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.46123042622e-13.
Allowing negative dual variable(s) as small as -3.43921505858e-13.
Allowing negative dual variable(s) as small as -5.20508983137e-13.
Allowing negative dual variable(s) as small as -5.23575974243e-13.
Solving took 4 GP solves and 2.75 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Beginning signomial solve.
Allowing negative dual variable(s) as small as -5.49438532865e-13.
Allowing negative dual variable(s) as small as -3.24928885881e-13.
Allowing negative dual variable(s) as small as -5.276369619e-13.
Allowing negative dual variable(s) as small as -5.20338980237e-13.
Solving took 4 GP solves and 2.72 seconds.
Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000
Allowing negative dual variable(s) as small as -8.56436449537e-13.
Allowing negative dual variable(s) as small as -7.72875687061e-13.
Allowing negative dual variable(s) as small as -7.38449232318e-13.
Allowing negative dual variable(s) as small as -7.41604694321e-13.
Allowing negative dual variable(s) as small as -7.41175350261e-13.
Allowing negative dual variable(s) as small as -1.52341073784e-12.
Allowing negative dual variable(s) as small as -1.04627786469e-12.
Allowing negative dual variable(s) as small as -1.06227353303e-12.
Allowing negative dual variable(s) as small as -1.06248007354e-12.
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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
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 -1.48224466555e-12.
Allowing negative dual variable(s) as small as -1.13588609005e-13.
Allowing negative dual variable(s) as small as -6.01927362121e-15.
Allowing negative dual variable(s) as small as -1.60394375733e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.52650241699e-14.
Allowing negative dual variable(s) as small as -1.08222987914e-12.
Solving took 4 GP solves and 2.36 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 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 1.61 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
Allowing negative dual variable(s) as small as -8.57014112454e-13.
Allowing negative dual variable(s) as small as -7.72726500842e-13.
Allowing negative dual variable(s) as small as -7.39320930865e-13.
Allowing negative dual variable(s) as small as -7.41162339835e-13.
Allowing negative dual variable(s) as small as -7.41588214448e-13.
Allowing negative dual variable(s) as small as -1.51704018271e-12.
Allowing negative dual variable(s) as small as -1.04852476528e-12.
Allowing negative dual variable(s) as small as -1.06169966482e-12.
Allowing negative dual variable(s) as small as -1.06107603173e-12.
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 = 21.769
speed at top of climb [m/s] = 26.550
design loiter speed [m/s] = 25.056
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 -1.48203931766e-12.
Allowing negative dual variable(s) as small as -1.14490231531e-13.
Allowing negative dual variable(s) as small as -6.13745165801e-15.
Allowing negative dual variable(s) as small as -1.60838356522e-13.
optimum loiter speed for min power, start of loiter [m/s] = 25.207
optimum loiter speed for min power, end of loiter [m/s] = 17.178
optimum cruise speed, inbound [m/s] = 36.034
optimum cruise speed, outbound [m/s] = 25.521
Beginning signomial solve.
Allowing negative dual variable(s) as small as -1.51349256266e-14.
Allowing negative dual variable(s) as small as -1.08164602362e-12.
Solving took 4 GP solves and 2.52 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 1078212.3036 but bound is 1000000.0000
Max Speed [m/s]: 74.35
Beginning signomial solve.
Solving took 4 GP solves and 1.54 seconds.
Max payload weight [lbf] = 27.446
Max take off weight [lbf] = 165.351
	

Standard Error