Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171025135916)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.06965474945e-14.
Allowing negative dual variable(s) as small as -1.20756573144e-12.
Allowing negative dual variable(s) as small as -1.13114162134e-12.
Allowing negative dual variable(s) as small as -1.13889366687e-12.
Solving took 4 GP solves and 7.97 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.84338478782e-14.
Allowing negative dual variable(s) as small as -1.18864727089e-12.
Allowing negative dual variable(s) as small as -1.14490665212e-12.
Allowing negative dual variable(s) as small as -1.12660748786e-12.
Solving took 4 GP solves and 2.36 seconds.
Allowing negative dual variable(s) as small as -1.56999153261e-12.
Allowing negative dual variable(s) as small as -3.96095222593e-12.
Allowing negative dual variable(s) as small as -1.78681548724e-12.
Allowing negative dual variable(s) as small as -2.08217037362e-12.
Allowing negative dual variable(s) as small as -2.08108356936e-12.
Allowing negative dual variable(s) as small as -4.70186606663e-13.
Allowing negative dual variable(s) as small as -8.93130838384e-13.
Allowing negative dual variable(s) as small as -9.41444838753e-13.
Allowing negative dual variable(s) as small as -9.4167262963e-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 -2.31805026563e-13.
Allowing negative dual variable(s) as small as -9.24776748235e-14.
Allowing negative dual variable(s) as small as -1.20050453953e-13.
Allowing negative dual variable(s) as small as -1.20447597209e-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 -9.61458582359e-13.
Allowing negative dual variable(s) as small as -2.0167800448e-12.
Allowing negative dual variable(s) as small as -1.2213981583e-14.
Allowing negative dual variable(s) as small as -1.76555126656e-14.
Solving took 4 GP solves and 2.54 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 3.1 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56968622128e-12.
Allowing negative dual variable(s) as small as -3.96074232439e-12.
Allowing negative dual variable(s) as small as -1.7869048255e-12.
Allowing negative dual variable(s) as small as -2.08315396183e-12.
Allowing negative dual variable(s) as small as -2.08089014769e-12.
Allowing negative dual variable(s) as small as -4.73864220432e-13.
Allowing negative dual variable(s) as small as -8.93431053965e-13.
Allowing negative dual variable(s) as small as -9.42179385725e-13.
Allowing negative dual variable(s) as small as -9.42588888886e-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 -2.35276208238e-13.
Allowing negative dual variable(s) as small as -9.26199221485e-14.
Allowing negative dual variable(s) as small as -1.20259704972e-13.
Allowing negative dual variable(s) as small as -1.19940515853e-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 -9.61389536468e-13.
Allowing negative dual variable(s) as small as -2.0166967547e-12.
Allowing negative dual variable(s) as small as -1.29163588259e-14.
Allowing negative dual variable(s) as small as -1.64714436146e-14.
Solving took 4 GP solves and 5.1 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 1.53 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error