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Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171016093549)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -4.42422530902e-12. Allowing negative dual variable(s) as small as -4.93609233349e-12. Allowing negative dual variable(s) as small as -4.76873965663e-12. Allowing negative dual variable(s) as small as -9.18278821038e-12. Solving took 4 GP solves and 2.51 seconds. Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.42422530902e-12. Allowing negative dual variable(s) as small as -4.93609233349e-12. Allowing negative dual variable(s) as small as -4.76873965663e-12. Allowing negative dual variable(s) as small as -9.18278821038e-12. Solving took 4 GP solves and 2.34 seconds. Warning: Variable [Re_Mission/Cruise/FlightSegment.1/AircraftPerf.1/TailAero.3_(0,)] could cause inaccurate result because it is above upper bound. Solution is 1155331.2270 but bound is 1000000.0000 Allowing negative dual variable(s) as small as -1.61293617351e-11. Allowing negative dual variable(s) as small as -6.11012629381e-12. Allowing negative dual variable(s) as small as -1.16702689179e-11. Allowing negative dual variable(s) as small as -6.59274718151e-12. Allowing negative dual variable(s) as small as -6.60738824765e-12. Allowing negative dual variable(s) as small as -1.10100370661e-11. Allowing negative dual variable(s) as small as -1.16824745407e-11. Allowing negative dual variable(s) as small as -1.10536612415e-11. Allowing negative dual variable(s) as small as -1.11136000576e-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 = 21.769 speed at top of climb [m/s] = 26.550 design loiter speed [m/s] = 25.056 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 -1.79908264935e-11. Allowing negative dual variable(s) as small as -6.27461819482e-12. Allowing negative dual variable(s) as small as -1.04086456251e-11. Allowing negative dual variable(s) as small as -1.04258197128e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.207 optimum loiter speed for min power, end of loiter [m/s] = 17.178 optimum cruise speed, inbound [m/s] = 36.034 optimum cruise speed, outbound [m/s] = 25.521 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.91623150625e-12. Allowing negative dual variable(s) as small as -2.30023010961e-13. Allowing negative dual variable(s) as small as -3.13912101671e-13. Allowing negative dual variable(s) as small as -9.07445567926e-14. Solving took 4 GP solves and 2.93 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 1078212.3036 but bound is 1000000.0000 Max Speed [m/s]: 74.35 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.91038787493e-11. Allowing negative dual variable(s) as small as -8.93094617357e-11. Allowing negative dual variable(s) as small as -8.9884532109e-11. Allowing negative dual variable(s) as small as -8.47861910888e-11. Solving took 4 GP solves and 1.98 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351 Allowing negative dual variable(s) as small as -1.61293617351e-11. Allowing negative dual variable(s) as small as -6.11012629381e-12. Allowing negative dual variable(s) as small as -1.16702689179e-11. Allowing negative dual variable(s) as small as -6.59274718151e-12. Allowing negative dual variable(s) as small as -6.60738824765e-12. Allowing negative dual variable(s) as small as -1.10100370661e-11. Allowing negative dual variable(s) as small as -1.16824745407e-11. Allowing negative dual variable(s) as small as -1.10536612415e-11. Allowing negative dual variable(s) as small as -1.11136000576e-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 = 21.769 speed at top of climb [m/s] = 26.550 design loiter speed [m/s] = 25.056 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 -1.79908264935e-11. Allowing negative dual variable(s) as small as -6.27461819482e-12. Allowing negative dual variable(s) as small as -1.04086456251e-11. Allowing negative dual variable(s) as small as -1.04258197128e-11. optimum loiter speed for min power, start of loiter [m/s] = 25.207 optimum loiter speed for min power, end of loiter [m/s] = 17.178 optimum cruise speed, inbound [m/s] = 36.034 optimum cruise speed, outbound [m/s] = 25.521 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.91623150625e-12. Allowing negative dual variable(s) as small as -2.30023010961e-13. Allowing negative dual variable(s) as small as -3.13912101671e-13. Allowing negative dual variable(s) as small as -9.07445567926e-14. Solving took 4 GP solves and 1.58 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 1078212.3036 but bound is 1000000.0000 Max Speed [m/s]: 74.35 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.91038787493e-11. Allowing negative dual variable(s) as small as -8.93094617357e-11. Allowing negative dual variable(s) as small as -8.9884532109e-11. Allowing negative dual variable(s) as small as -8.47861910888e-11. Solving took 4 GP solves and 2 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351