Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018091746)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.62602393628e-14.
Allowing negative dual variable(s) as small as -1.17650637496e-12.
Allowing negative dual variable(s) as small as -1.14217446265e-12.
Allowing negative dual variable(s) as small as -1.12922822135e-12.
Solving took 4 GP solves and 1.68 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.63070768967e-14.
Allowing negative dual variable(s) as small as -1.19016515393e-12.
Allowing negative dual variable(s) as small as -1.12920610362e-12.
Allowing negative dual variable(s) as small as -1.1422321422e-12.
Solving took 4 GP solves and 3.83 seconds.
Allowing negative dual variable(s) as small as -1.56932279671e-12.
Allowing negative dual variable(s) as small as -3.96094528704e-12.
Allowing negative dual variable(s) as small as -1.78698809222e-12.
Allowing negative dual variable(s) as small as -2.08210358676e-12.
Allowing negative dual variable(s) as small as -2.08057356066e-12.
Allowing negative dual variable(s) as small as -4.78779342561e-13.
Allowing negative dual variable(s) as small as -8.93815403635e-13.
Allowing negative dual variable(s) as small as -9.40817736217e-13.
Allowing negative dual variable(s) as small as -9.41925573997e-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 -2.32869496256e-13.
Allowing negative dual variable(s) as small as -9.26667596823e-14.
Allowing negative dual variable(s) as small as -1.19909941351e-13.
Allowing negative dual variable(s) as small as -1.20000363812e-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 -9.61907356932e-13.
Allowing negative dual variable(s) as small as -2.01708165446e-12.
Allowing negative dual variable(s) as small as -1.24888135459e-14.
Allowing negative dual variable(s) as small as -1.76953489428e-14.
Solving took 4 GP solves and 3.96 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
Allowing negative dual variable(s) as small as -1.56939912455e-12.
Allowing negative dual variable(s) as small as -3.96097737942e-12.
Allowing negative dual variable(s) as small as -1.78717717708e-12.
Allowing negative dual variable(s) as small as -2.08247741967e-12.
Allowing negative dual variable(s) as small as -2.08107923255e-12.
Allowing negative dual variable(s) as small as -4.7450173131e-13.
Allowing negative dual variable(s) as small as -8.92182161483e-13.
Allowing negative dual variable(s) as small as -9.41767063639e-13.
Allowing negative dual variable(s) as small as -9.43671464755e-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 -2.36067025303e-13.
Allowing negative dual variable(s) as small as -9.27447138185e-14.
Allowing negative dual variable(s) as small as -1.20433611001e-13.
Allowing negative dual variable(s) as small as -1.19171274411e-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 -9.61428691202e-13.
Allowing negative dual variable(s) as small as -2.01685582598e-12.
Allowing negative dual variable(s) as small as -1.34833570692e-14.
Allowing negative dual variable(s) as small as -1.71900700199e-14.
Solving took 4 GP solves and 7.18 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 2.1 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error