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Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018111337)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.07391760415e-11. Allowing negative dual variable(s) as small as -1.59918779608e-12. Allowing negative dual variable(s) as small as -1.62213124877e-12. Allowing negative dual variable(s) as small as -1.61967661505e-12. Solving took 4 GP solves and 4.77 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.07426606673e-11. Allowing negative dual variable(s) as small as -1.60183194833e-12. Allowing negative dual variable(s) as small as -1.5308492321e-12. Allowing negative dual variable(s) as small as -1.46860345066e-12. Solving took 4 GP solves and 5.34 seconds. Allowing negative dual variable(s) as small as -7.73001801457e-12. Allowing negative dual variable(s) as small as -3.41769598733e-11. Allowing negative dual variable(s) as small as -2.09315620392e-11. Allowing negative dual variable(s) as small as -2.11249767679e-11. Allowing negative dual variable(s) as small as -2.14122261588e-11. Allowing negative dual variable(s) as small as -4.94431535644e-12. Allowing negative dual variable(s) as small as -1.04714935724e-11. Allowing negative dual variable(s) as small as -5.89531461842e-12. Allowing negative dual variable(s) as small as -1.10750157959e-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 = 21.712 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 -2.77663374064e-12. Allowing negative dual variable(s) as small as -7.11332327676e-12. Allowing negative dual variable(s) as small as -1.34990854215e-11. Allowing negative dual variable(s) as small as -1.37363711985e-11. 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 -3.42465561948e-11. Allowing negative dual variable(s) as small as -3.57352074283e-11. Allowing negative dual variable(s) as small as -3.97063812773e-13. Allowing negative dual variable(s) as small as -5.67077695976e-11. Solving took 4 GP solves and 5.04 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.10278148261e-13. Allowing negative dual variable(s) as small as -1.80550687248e-11. Allowing negative dual variable(s) as small as -7.28667985325e-11. Allowing negative dual variable(s) as small as -1.43014259289e-11. Solving took 4 GP solves and 3.69 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.73742181437e-12. Allowing negative dual variable(s) as small as -3.4172595309e-11. Allowing negative dual variable(s) as small as -2.09180867072e-11. Allowing negative dual variable(s) as small as -2.11583320309e-11. Allowing negative dual variable(s) as small as -2.14014569955e-11. Allowing negative dual variable(s) as small as -4.88867475147e-12. Allowing negative dual variable(s) as small as -1.04708393648e-11. Allowing negative dual variable(s) as small as -5.89391979233e-12. Allowing negative dual variable(s) as small as -1.10738221978e-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 = 21.712 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 -2.76014497716e-12. Allowing negative dual variable(s) as small as -7.11425222118e-12. Allowing negative dual variable(s) as small as -1.3497217558e-11. Allowing negative dual variable(s) as small as -1.37355024273e-11. 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 -3.42442499587e-11. Allowing negative dual variable(s) as small as -3.57327763705e-11. Allowing negative dual variable(s) as small as -3.97782224826e-13. Allowing negative dual variable(s) as small as -5.67066172084e-11. Solving took 4 GP solves and 243 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.11007165801e-13. Allowing negative dual variable(s) as small as -1.80594137734e-11. Allowing negative dual variable(s) as small as -7.28696105193e-11. Allowing negative dual variable(s) as small as -1.43031749639e-11. Solving took 4 GP solves and 97.9 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531