Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171025135745)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.60746239509e-14. Allowing negative dual variable(s) as small as -1.17544212211e-12. Allowing negative dual variable(s) as small as -1.13401519078e-12. Allowing negative dual variable(s) as small as -1.14676107152e-12. Solving took 4 GP solves and 2.9 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.641853288e-14. Allowing negative dual variable(s) as small as -1.17108579778e-12. Allowing negative dual variable(s) as small as -1.1347537493e-12. Allowing negative dual variable(s) as small as -1.14664831449e-12. Solving took 4 GP solves and 3.23 seconds. Allowing negative dual variable(s) as small as -1.56940606344e-12. Allowing negative dual variable(s) as small as -3.96053329021e-12. Allowing negative dual variable(s) as small as -1.78701411307e-12. Allowing negative dual variable(s) as small as -2.08250951206e-12. Allowing negative dual variable(s) as small as -2.08075223718e-12. Allowing negative dual variable(s) as small as -4.72263504345e-13. Allowing negative dual variable(s) as small as -8.92169042636e-13. Allowing negative dual variable(s) as small as -9.40487596655e-13. Allowing negative dual variable(s) as small as -9.42551375491e-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 -2.38329321556e-13. Allowing negative dual variable(s) as small as -9.30038381378e-14. Allowing negative dual variable(s) as small as -1.19231230791e-13. Allowing negative dual variable(s) as small as -1.19818001007e-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 -9.61280156351e-13. Allowing negative dual variable(s) as small as -2.01620264848e-12. Allowing negative dual variable(s) as small as -1.29247866978e-14. Allowing negative dual variable(s) as small as -1.7343430523e-14. Solving took 4 GP solves and 3.56 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 2.3 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56955698438e-12. Allowing negative dual variable(s) as small as -3.9602071622e-12. Allowing negative dual variable(s) as small as -1.78685018171e-12. Allowing negative dual variable(s) as small as -2.08236726473e-12. Allowing negative dual variable(s) as small as -2.08093004633e-12. Allowing negative dual variable(s) as small as -4.77057412671e-13. Allowing negative dual variable(s) as small as -8.92114507267e-13. Allowing negative dual variable(s) as small as -9.42305803699e-13. Allowing negative dual variable(s) as small as -9.42792393634e-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 -2.34431614746e-13. Allowing negative dual variable(s) as small as -9.17051807756e-14. Allowing negative dual variable(s) as small as -1.19718471248e-13. Allowing negative dual variable(s) as small as -1.20805492346e-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 -9.60497872932e-13. Allowing negative dual variable(s) as small as -2.01671884638e-12. Allowing negative dual variable(s) as small as -1.31153621759e-14. Allowing negative dual variable(s) as small as -1.77151221858e-14. Solving took 4 GP solves and 3.51 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 1.85 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531