Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171016202509)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.54887210969e-14. Allowing negative dual variable(s) as small as -1.17742100791e-12. Allowing negative dual variable(s) as small as -1.14131100404e-12. Allowing negative dual variable(s) as small as -1.14081183736e-12. Solving took 4 GP solves and 5.21 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.01646122075e-13. Allowing negative dual variable(s) as small as -1.17227625177e-12. Allowing negative dual variable(s) as small as -1.1354112095e-12. Allowing negative dual variable(s) as small as -1.12470406252e-12. Solving took 4 GP solves and 2.01 seconds. Allowing negative dual variable(s) as small as -1.56934534812e-12. Allowing negative dual variable(s) as small as -3.9608871738e-12. Allowing negative dual variable(s) as small as -1.78670012813e-12. Allowing negative dual variable(s) as small as -2.08236899946e-12. Allowing negative dual variable(s) as small as -2.08074529828e-12. Allowing negative dual variable(s) as small as -4.72235098248e-13. Allowing negative dual variable(s) as small as -8.93242728048e-13. Allowing negative dual variable(s) as small as -9.4073923998e-13. Allowing negative dual variable(s) as small as -9.44143309541e-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 -2.28685343232e-13. Allowing negative dual variable(s) as small as -9.27694336281e-14. Allowing negative dual variable(s) as small as -1.19352986695e-13. Allowing negative dual variable(s) as small as -1.20252115557e-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 -9.61398786492e-13. Allowing negative dual variable(s) as small as -2.01783224596e-12. Allowing negative dual variable(s) as small as -1.27258002355e-14. Allowing negative dual variable(s) as small as -1.76552011693e-14. Solving took 4 GP solves and 3.12 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 4.31 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56981459082e-12. Allowing negative dual variable(s) as small as -3.96070242575e-12. Allowing negative dual variable(s) as small as -1.78650670646e-12. Allowing negative dual variable(s) as small as -2.08240716337e-12. Allowing negative dual variable(s) as small as -2.08098815957e-12. Allowing negative dual variable(s) as small as -4.72637554094e-13. Allowing negative dual variable(s) as small as -8.93307563338e-13. Allowing negative dual variable(s) as small as -9.41251200245e-13. Allowing negative dual variable(s) as small as -9.43594594821e-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 -2.37099619452e-13. Allowing negative dual variable(s) as small as -9.19345979553e-14. Allowing negative dual variable(s) as small as -1.19538168426e-13. Allowing negative dual variable(s) as small as -1.20402494398e-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 -9.61399790861e-13. Allowing negative dual variable(s) as small as -2.01627488438e-12. Allowing negative dual variable(s) as small as -1.32873863089e-14. Allowing negative dual variable(s) as small as -1.76514913238e-14. Solving took 4 GP solves and 22.8 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 5.68 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531