Passed

gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171025135807)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.7302374491e-14.
Allowing negative dual variable(s) as small as -1.20174009632e-12.
Allowing negative dual variable(s) as small as -1.1483188532e-12.
Allowing negative dual variable(s) as small as -1.14169654633e-12.
Solving took 4 GP solves and 37.3 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.52662428111e-14.
Allowing negative dual variable(s) as small as -1.19322780823e-12.
Allowing negative dual variable(s) as small as -1.13118932624e-12.
Allowing negative dual variable(s) as small as -1.14648785257e-12.
Solving took 4 GP solves and 21.1 seconds.
Allowing negative dual variable(s) as small as -1.56905825138e-12.
Allowing negative dual variable(s) as small as -3.96106671768e-12.
Allowing negative dual variable(s) as small as -1.7867686497e-12.
Allowing negative dual variable(s) as small as -2.0824088981e-12.
Allowing negative dual variable(s) as small as -2.08112867217e-12.
Allowing negative dual variable(s) as small as -4.72213197364e-13.
Allowing negative dual variable(s) as small as -8.93349847222e-13.
Allowing negative dual variable(s) as small as -9.43725024342e-13.
Allowing negative dual variable(s) as small as -9.42560374369e-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 -2.3328084256e-13.
Allowing negative dual variable(s) as small as -9.1588629042e-14.
Allowing negative dual variable(s) as small as -1.20460173954e-13.
Allowing negative dual variable(s) as small as -1.20720924576e-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 -9.61371811669e-13.
Allowing negative dual variable(s) as small as -2.01666365059e-12.
Allowing negative dual variable(s) as small as -1.28484577002e-14.
Allowing negative dual variable(s) as small as -1.71685415128e-14.
Solving took 4 GP solves and 21 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 13.3 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56970790532e-12.
Allowing negative dual variable(s) as small as -3.9604838506e-12.
Allowing negative dual variable(s) as small as -1.78663073919e-12.
Allowing negative dual variable(s) as small as -2.08213567915e-12.
Allowing negative dual variable(s) as small as -2.08115729511e-12.
Allowing negative dual variable(s) as small as -4.70889386511e-13.
Allowing negative dual variable(s) as small as -8.93604526313e-13.
Allowing negative dual variable(s) as small as -9.4079919636e-13.
Allowing negative dual variable(s) as small as -9.42605151918e-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 -2.36548194227e-13.
Allowing negative dual variable(s) as small as -9.27762641018e-14.
Allowing negative dual variable(s) as small as -1.19043121714e-13.
Allowing negative dual variable(s) as small as -1.20717129869e-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 -9.60913541222e-13.
Allowing negative dual variable(s) as small as -2.01617827659e-12.
Allowing negative dual variable(s) as small as -1.30784161869e-14.
Allowing negative dual variable(s) as small as -1.75533682743e-14.
Solving took 4 GP solves and 22.8 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 15 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error