Passed

gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018105736)

Standard Output

Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.25301502086e-14.
Allowing negative dual variable(s) as small as -1.17557135901e-12.
Allowing negative dual variable(s) as small as -1.14147103228e-12.
Allowing negative dual variable(s) as small as -1.13468913085e-12.
Solving took 4 GP solves and 2.08 seconds.
Beginning signomial solve.
Allowing negative dual variable(s) as small as -9.93311335962e-14.
Allowing negative dual variable(s) as small as -1.18021564743e-12.
Allowing negative dual variable(s) as small as -1.13784372549e-12.
Allowing negative dual variable(s) as small as -1.15457686814e-12.
Solving took 4 GP solves and 1.73 seconds.
Allowing negative dual variable(s) as small as -1.56936182799e-12.
Allowing negative dual variable(s) as small as -3.9610528399e-12.
Allowing negative dual variable(s) as small as -1.7870089089e-12.
Allowing negative dual variable(s) as small as -2.08283997688e-12.
Allowing negative dual variable(s) as small as -2.08082683029e-12.
Allowing negative dual variable(s) as small as -4.7236585303e-13.
Allowing negative dual variable(s) as small as -8.9273488775e-13.
Allowing negative dual variable(s) as small as -9.41451669227e-13.
Allowing negative dual variable(s) as small as -9.42798248325e-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 -2.34568874741e-13.
Allowing negative dual variable(s) as small as -9.36918728364e-14.
Allowing negative dual variable(s) as small as -1.18942290912e-13.
Allowing negative dual variable(s) as small as -1.19173334395e-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 -9.61260998795e-13.
Allowing negative dual variable(s) as small as -2.01714649679e-12.
Allowing negative dual variable(s) as small as -1.27002234934e-14.
Allowing negative dual variable(s) as small as -1.78541864669e-14.
Solving took 4 GP solves and 2.76 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 2.01 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
Allowing negative dual variable(s) as small as -1.56945376834e-12.
Allowing negative dual variable(s) as small as -3.96119855667e-12.
Allowing negative dual variable(s) as small as -1.78681895668e-12.
Allowing negative dual variable(s) as small as -2.08201771795e-12.
Allowing negative dual variable(s) as small as -2.0810237214e-12.
Allowing negative dual variable(s) as small as -4.7455680878e-13.
Allowing negative dual variable(s) as small as -8.94520243468e-13.
Allowing negative dual variable(s) as small as -9.4151292665e-13.
Allowing negative dual variable(s) as small as -9.42716174221e-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 -2.34601834487e-13.
Allowing negative dual variable(s) as small as -9.23334759345e-14.
Allowing negative dual variable(s) as small as -1.19457070104e-13.
Allowing negative dual variable(s) as small as -1.2025385028e-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 -9.60729238922e-13.
Allowing negative dual variable(s) as small as -2.01691029777e-12.
Allowing negative dual variable(s) as small as -1.28456150576e-14.
Allowing negative dual variable(s) as small as -1.75237750607e-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 1.88 seconds.
Max payload weight [lbf] = 26.860
Max take off weight [lbf] = 164.531
	

Standard Error