Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018110753)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.82109359116e-14.
Allowing negative dual variable(s) as small as -1.20098766002e-12.
Allowing negative dual variable(s) as small as -1.13344533412e-12.
Allowing negative dual variable(s) as small as -1.13336727156e-12.
Solving took 4 GP solves and 2.23 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.83774693653e-14.
Allowing negative dual variable(s) as small as -1.18665103785e-12.
Allowing negative dual variable(s) as small as -1.13640520605e-12.
Allowing negative dual variable(s) as small as -1.1256091545e-12.
Solving took 4 GP solves and 2.05 seconds.
Allowing negative dual variable(s) as small as -1.56935575646e-12.
Allowing negative dual variable(s) as small as -3.9607648758e-12.
Allowing negative dual variable(s) as small as -1.78750157037e-12.
Allowing negative dual variable(s) as small as -2.08239848976e-12.
Allowing negative dual variable(s) as small as -2.08095606719e-12.
Allowing negative dual variable(s) as small as -4.73684026031e-13.
Allowing negative dual variable(s) as small as -8.92673088226e-13.
Allowing negative dual variable(s) as small as -9.40558178217e-13.
Allowing negative dual variable(s) as small as -9.43293620298e-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 -2.38523176904e-13.
Allowing negative dual variable(s) as small as -9.1885049916e-14.
Allowing negative dual variable(s) as small as -1.2078760301e-13.
Allowing negative dual variable(s) as small as -1.1972454278e-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 -9.6098190398e-13.
Allowing negative dual variable(s) as small as -2.0170853723e-12.
Allowing negative dual variable(s) as small as -1.23793879006e-14.
Allowing negative dual variable(s) as small as -1.70982214728e-14.
Solving took 4 GP solves and 2.75 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
Allowing negative dual variable(s) as small as -1.56958213787e-12.
Allowing negative dual variable(s) as small as -3.9605246166e-12.
Allowing negative dual variable(s) as small as -1.78657783012e-12.
Allowing negative dual variable(s) as small as -2.08217731251e-12.
Allowing negative dual variable(s) as small as -2.08069585866e-12.
Allowing negative dual variable(s) as small as -4.71395708926e-13.
Allowing negative dual variable(s) as small as -8.93394950033e-13.
Allowing negative dual variable(s) as small as -9.42780033729e-13.
Allowing negative dual variable(s) as small as -9.42525246218e-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 -2.31551323254e-13.
Allowing negative dual variable(s) as small as -9.29851898604e-14.
Allowing negative dual variable(s) as small as -1.18552411811e-13.
Allowing negative dual variable(s) as small as -1.21156665429e-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 -9.62081417544e-13.
Allowing negative dual variable(s) as small as -2.01675802604e-12.
Allowing negative dual variable(s) as small as -1.23215023042e-14.
Allowing negative dual variable(s) as small as -1.76472020019e-14.
Solving took 4 GP solves and 3.15 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 1.87 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error