Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171016200642)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.6375598474e-14. Allowing negative dual variable(s) as small as -1.18723217021e-12. Allowing negative dual variable(s) as small as -1.13446448416e-12. Allowing negative dual variable(s) as small as -1.1117764695e-12. Solving took 4 GP solves and 7.34 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.52779521946e-14. Allowing negative dual variable(s) as small as -1.18534218899e-12. Allowing negative dual variable(s) as small as -1.13956023437e-12. Allowing negative dual variable(s) as small as -1.13494847201e-12. Solving took 4 GP solves and 2.13 seconds. Allowing negative dual variable(s) as small as -1.57007306462e-12. Allowing negative dual variable(s) as small as -3.96046910545e-12. Allowing negative dual variable(s) as small as -1.787378405e-12. Allowing negative dual variable(s) as small as -2.08232129456e-12. Allowing negative dual variable(s) as small as -2.08063687807e-12. Allowing negative dual variable(s) as small as -4.74151100327e-13. Allowing negative dual variable(s) as small as -8.92368752677e-13. Allowing negative dual variable(s) as small as -9.41076535275e-13. Allowing negative dual variable(s) as small as -9.42659036766e-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 -2.39716449815e-13. Allowing negative dual variable(s) as small as -9.32167754444e-14. Allowing negative dual variable(s) as small as -1.19906363484e-13. Allowing negative dual variable(s) as small as -1.19852478636e-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 -9.6116007609e-13. Allowing negative dual variable(s) as small as -2.01709978735e-12. Allowing negative dual variable(s) as small as -1.26152400954e-14. Allowing negative dual variable(s) as small as -1.78318643429e-14. Solving took 4 GP solves and 3.73 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 4.56 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56920830496e-12. Allowing negative dual variable(s) as small as -3.96091406202e-12. Allowing negative dual variable(s) as small as -1.78683717128e-12. Allowing negative dual variable(s) as small as -2.08237680571e-12. Allowing negative dual variable(s) as small as -2.08071407326e-12. Allowing negative dual variable(s) as small as -4.77189251655e-13. Allowing negative dual variable(s) as small as -8.93292059247e-13. Allowing negative dual variable(s) as small as -9.40585174851e-13. Allowing negative dual variable(s) as small as -9.42892790755e-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 -2.35934752638e-13. Allowing negative dual variable(s) as small as -9.29164514427e-14. Allowing negative dual variable(s) as small as -1.19110450669e-13. Allowing negative dual variable(s) as small as -1.19305715481e-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 -9.61286022478e-13. Allowing negative dual variable(s) as small as -2.01716500277e-12. Allowing negative dual variable(s) as small as -1.293366895e-14. Allowing negative dual variable(s) as small as -1.72812288174e-14. Solving took 4 GP solves and 4.89 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 3.72 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531