Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171014230954)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.56234312082e-13. Allowing negative dual variable(s) as small as -3.08241713404e-13. Allowing negative dual variable(s) as small as -5.43759048205e-13. Allowing negative dual variable(s) as small as -5.17845748921e-13. Solving took 4 GP solves and 2.17 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 -5.40948362493e-13. Allowing negative dual variable(s) as small as -3.43379404771e-13. Allowing negative dual variable(s) as small as -5.308808948e-13. Allowing negative dual variable(s) as small as -5.26388828359e-13. Solving took 4 GP solves and 4.71 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 -8.57262177911e-13. Allowing negative dual variable(s) as small as -7.71942405831e-13. Allowing negative dual variable(s) as small as -7.3816560503e-13. Allowing negative dual variable(s) as small as -7.41321067033e-13. Allowing negative dual variable(s) as small as -7.41008816807e-13. Allowing negative dual variable(s) as small as -1.51350308154e-12. Allowing negative dual variable(s) as small as -1.04774348919e-12. Allowing negative dual variable(s) as small as -1.061224459e-12. Allowing negative dual variable(s) as small as -1.06289315457e-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 -1.48288542903e-12. Allowing negative dual variable(s) as small as -1.14034758199e-13. Allowing negative dual variable(s) as small as -6.34410059208e-15. Allowing negative dual variable(s) as small as -1.59590981923e-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 -1.46377593206e-14. Allowing negative dual variable(s) as small as -1.08079234699e-12. Solving took 4 GP solves and 7.88 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 2.7 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351 Allowing negative dual variable(s) as small as -8.57234422336e-13. Allowing negative dual variable(s) as small as -7.72004855876e-13. Allowing negative dual variable(s) as small as -7.38476120532e-13. Allowing negative dual variable(s) as small as -7.41403466398e-13. Allowing negative dual variable(s) as small as -7.41256882264e-13. Allowing negative dual variable(s) as small as -1.52006011944e-12. Allowing negative dual variable(s) as small as -1.0467321454e-12. Allowing negative dual variable(s) as small as -1.06134838331e-12. Allowing negative dual variable(s) as small as -1.06128051226e-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 -1.47943636508e-12. Allowing negative dual variable(s) as small as -1.1372099009e-13. Allowing negative dual variable(s) as small as -6.71793350115e-15. Allowing negative dual variable(s) as small as -1.61210129447e-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 -1.53921091816e-14. Allowing negative dual variable(s) as small as -1.0811970672e-12. Solving took 4 GP solves and 22.4 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 4.58 seconds. Max payload weight [lbf] = 27.446 Max take off weight [lbf] = 165.351