Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171017121811)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.50190447158e-14.
Allowing negative dual variable(s) as small as -1.19836215604e-12.
Allowing negative dual variable(s) as small as -1.13664589893e-12.
Allowing negative dual variable(s) as small as -1.13907884861e-12.
Solving took 4 GP solves and 23.4 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.55377270351e-14.
Allowing negative dual variable(s) as small as -1.19775847227e-12.
Allowing negative dual variable(s) as small as -1.14401543794e-12.
Allowing negative dual variable(s) as small as -1.14260380671e-12.
Solving took 4 GP solves and 26.1 seconds.
Allowing negative dual variable(s) as small as -1.569524892e-12.
Allowing negative dual variable(s) as small as -3.96128355812e-12.
Allowing negative dual variable(s) as small as -1.78702105197e-12.
Allowing negative dual variable(s) as small as -2.08188761369e-12.
Allowing negative dual variable(s) as small as -2.08132990009e-12.
Allowing negative dual variable(s) as small as -4.73509686322e-13.
Allowing negative dual variable(s) as small as -8.93039982242e-13.
Allowing negative dual variable(s) as small as -9.40689149839e-13.
Allowing negative dual variable(s) as small as -9.42569156406e-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 -2.3443855364e-13.
Allowing negative dual variable(s) as small as -9.31040184185e-14.
Allowing negative dual variable(s) as small as -1.19332278434e-13.
Allowing negative dual variable(s) as small as -1.20677556489e-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 -9.62473693748e-13.
Allowing negative dual variable(s) as small as -2.017069356e-12.
Allowing negative dual variable(s) as small as -1.31117161225e-14.
Allowing negative dual variable(s) as small as -1.74486868605e-14.
Solving took 4 GP solves and 3.95 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 -1.56927682654e-12.
Allowing negative dual variable(s) as small as -3.961086667e-12.
Allowing negative dual variable(s) as small as -1.78683023239e-12.
Allowing negative dual variable(s) as small as -2.08267517815e-12.
Allowing negative dual variable(s) as small as -2.08109484506e-12.
Allowing negative dual variable(s) as small as -4.70701819535e-13.
Allowing negative dual variable(s) as small as -8.94507666722e-13.
Allowing negative dual variable(s) as small as -9.40551456163e-13.
Allowing negative dual variable(s) as small as -9.43441830735e-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 -2.32549656615e-13.
Allowing negative dual variable(s) as small as -9.19181180822e-14.
Allowing negative dual variable(s) as small as -1.19120208489e-13.
Allowing negative dual variable(s) as small as -1.19733541658e-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 -9.61226452768e-13.
Allowing negative dual variable(s) as small as -2.01649058174e-12.
Allowing negative dual variable(s) as small as -1.29896229406e-14.
Allowing negative dual variable(s) as small as -1.77988019471e-14.
Solving took 4 GP solves and 5.31 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 1.79 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error