Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171011221930)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.46123042622e-13. Allowing negative dual variable(s) as small as -3.43921505858e-13. Allowing negative dual variable(s) as small as -5.20508983137e-13. Allowing negative dual variable(s) as small as -5.23575974243e-13. Solving took 4 GP solves and 2.75 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 -5.49438532865e-13. Allowing negative dual variable(s) as small as -3.24928885881e-13. Allowing negative dual variable(s) as small as -5.276369619e-13. Allowing negative dual variable(s) as small as -5.20338980237e-13. Solving took 4 GP solves and 2.72 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 -8.56436449537e-13. Allowing negative dual variable(s) as small as -7.72875687061e-13. Allowing negative dual variable(s) as small as -7.38449232318e-13. Allowing negative dual variable(s) as small as -7.41604694321e-13. Allowing negative dual variable(s) as small as -7.41175350261e-13. Allowing negative dual variable(s) as small as -1.52341073784e-12. Allowing negative dual variable(s) as small as -1.04627786469e-12. Allowing negative dual variable(s) as small as -1.06227353303e-12. Allowing negative dual variable(s) as small as -1.06248007354e-12. 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 -1.48224466555e-12. Allowing negative dual variable(s) as small as -1.13588609005e-13. Allowing negative dual variable(s) as small as -6.01927362121e-15. Allowing negative dual variable(s) as small as -1.60394375733e-13. 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 -1.52650241699e-14. Allowing negative dual variable(s) as small as -1.08222987914e-12. Solving took 4 GP solves and 2.36 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. Solving took 4 GP solves and 1.61 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351 Allowing negative dual variable(s) as small as -8.57014112454e-13. Allowing negative dual variable(s) as small as -7.72726500842e-13. Allowing negative dual variable(s) as small as -7.39320930865e-13. Allowing negative dual variable(s) as small as -7.41162339835e-13. Allowing negative dual variable(s) as small as -7.41588214448e-13. Allowing negative dual variable(s) as small as -1.51704018271e-12. Allowing negative dual variable(s) as small as -1.04852476528e-12. Allowing negative dual variable(s) as small as -1.06169966482e-12. Allowing negative dual variable(s) as small as -1.06107603173e-12. 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 -1.48203931766e-12. Allowing negative dual variable(s) as small as -1.14490231531e-13. Allowing negative dual variable(s) as small as -6.13745165801e-15. Allowing negative dual variable(s) as small as -1.60838356522e-13. 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 -1.51349256266e-14. Allowing negative dual variable(s) as small as -1.08164602362e-12. Solving took 4 GP solves and 2.52 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. Solving took 4 GP solves and 1.54 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351