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Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171018120427)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.10344523917e-11. Allowing negative dual variable(s) as small as -3.03912320657e-12. Allowing negative dual variable(s) as small as -1.62266944673e-12. Allowing negative dual variable(s) as small as -3.085031796e-12. Solving took 4 GP solves and 5.43 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.09757137874e-11. Allowing negative dual variable(s) as small as -1.59501014826e-12. Allowing negative dual variable(s) as small as -1.37288574606e-12. Allowing negative dual variable(s) as small as -3.09799234877e-12. Solving took 4 GP solves and 1.48 seconds. Allowing negative dual variable(s) as small as -7.73846958735e-12. Allowing negative dual variable(s) as small as -3.41464426179e-11. Allowing negative dual variable(s) as small as -2.09146797103e-11. Allowing negative dual variable(s) as small as -2.11311107501e-11. Allowing negative dual variable(s) as small as -2.13579709474e-11. Allowing negative dual variable(s) as small as -4.89465781274e-12. Allowing negative dual variable(s) as small as -1.04709270768e-11. Allowing negative dual variable(s) as small as -5.89326200687e-12. Allowing negative dual variable(s) as small as -1.10767819613e-11. 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 -2.74137917228e-12. Allowing negative dual variable(s) as small as -7.11367596773e-12. Allowing negative dual variable(s) as small as -1.34972557219e-11. Allowing negative dual variable(s) as small as -1.37366447427e-11. 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 -3.42466548707e-11. Allowing negative dual variable(s) as small as -3.57291137673e-11. Allowing negative dual variable(s) as small as -3.97473763802e-13. Allowing negative dual variable(s) as small as -5.67081642626e-11. Solving took 4 GP solves and 1.87 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.02196071586e-13. Allowing negative dual variable(s) as small as -1.80542334555e-11. Allowing negative dual variable(s) as small as -7.28754513332e-11. Allowing negative dual variable(s) as small as -1.43014254952e-11. Solving took 4 GP solves and 1.63 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.71900598995e-12. Allowing negative dual variable(s) as small as -3.41768696677e-11. Allowing negative dual variable(s) as small as -2.09293346543e-11. Allowing negative dual variable(s) as small as -2.10999481776e-11. Allowing negative dual variable(s) as small as -2.13895567924e-11. Allowing negative dual variable(s) as small as -4.89435792242e-12. Allowing negative dual variable(s) as small as -1.0470655701e-11. Allowing negative dual variable(s) as small as -5.89492669088e-12. Allowing negative dual variable(s) as small as -1.10752228786e-11. 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 -2.74623986746e-12. Allowing negative dual variable(s) as small as -7.11388988082e-12. Allowing negative dual variable(s) as small as -1.34982455985e-11. Allowing negative dual variable(s) as small as -1.37369265268e-11. 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 -3.42445695129e-11. Allowing negative dual variable(s) as small as -3.57327037881e-11. Allowing negative dual variable(s) as small as -3.97523662301e-13. Allowing negative dual variable(s) as small as -5.67109888029e-11. Solving took 4 GP solves and 2.25 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.08514801847e-13. Allowing negative dual variable(s) as small as -1.80548974209e-11. Allowing negative dual variable(s) as small as -7.28742274858e-11. Allowing negative dual variable(s) as small as -1.43010373509e-11. Solving took 4 GP solves and 2.05 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531