Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018110828)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.6451492626e-14. Allowing negative dual variable(s) as small as -1.1903178096e-12. Allowing negative dual variable(s) as small as -1.13790660922e-12. Allowing negative dual variable(s) as small as -1.13608558325e-12. Solving took 4 GP solves and 27.4 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.42058930864e-14. Allowing negative dual variable(s) as small as -1.1918842649e-12. Allowing negative dual variable(s) as small as -1.15241236692e-12. Allowing negative dual variable(s) as small as -1.14765575515e-12. Solving took 4 GP solves and 30.4 seconds. Allowing negative dual variable(s) as small as -1.56932713352e-12. Allowing negative dual variable(s) as small as -3.96075446746e-12. Allowing negative dual variable(s) as small as -1.78743478352e-12. Allowing negative dual variable(s) as small as -2.08265869828e-12. Allowing negative dual variable(s) as small as -2.0810714263e-12. Allowing negative dual variable(s) as small as -4.69092429831e-13. Allowing negative dual variable(s) as small as -8.91690692638e-13. Allowing negative dual variable(s) as small as -9.41326769137e-13. Allowing negative dual variable(s) as small as -9.42388636745e-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 -2.27294528685e-13. Allowing negative dual variable(s) as small as -9.21385363839e-14. Allowing negative dual variable(s) as small as -1.21044884185e-13. Allowing negative dual variable(s) as small as -1.21578528495e-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 -9.61294109313e-13. Allowing negative dual variable(s) as small as -2.016644311e-12. Allowing negative dual variable(s) as small as -1.32683605725e-14. Allowing negative dual variable(s) as small as -1.7050543947e-14. Solving took 4 GP solves and 7.23 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 16.1 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56958560732e-12. Allowing negative dual variable(s) as small as -3.96093921551e-12. Allowing negative dual variable(s) as small as -1.78641389875e-12. Allowing negative dual variable(s) as small as -2.08245400091e-12. Allowing negative dual variable(s) as small as -2.08044605848e-12. Allowing negative dual variable(s) as small as -4.72975608332e-13. Allowing negative dual variable(s) as small as -8.94017932601e-13. Allowing negative dual variable(s) as small as -9.41570389365e-13. Allowing negative dual variable(s) as small as -9.42493587515e-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 -2.36618884208e-13. Allowing negative dual variable(s) as small as -9.12046046325e-14. Allowing negative dual variable(s) as small as -1.19826999885e-13. Allowing negative dual variable(s) as small as -1.20144779542e-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 -9.61220657157e-13. Allowing negative dual variable(s) as small as -2.01615843564e-12. Allowing negative dual variable(s) as small as -1.33570264461e-14. Allowing negative dual variable(s) as small as -1.71804923007e-14. Solving took 4 GP solves and 26.4 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 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 3.26 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531