Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180110084330)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.952935205385865e-13. Allowing negative dual variable(s) as small as -4.4202380471147773e-13. Allowing negative dual variable(s) as small as -8.173453233673023e-14. Allowing negative dual variable(s) as small as -8.380210587966008e-14. Solving took 4 GP solves and 225 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.220367986693894e-13. Allowing negative dual variable(s) as small as -4.952084749210162e-13. Allowing negative dual variable(s) as small as -7.717286011621471e-14. Allowing negative dual variable(s) as small as -8.22224233143487e-14. Solving took 4 GP solves and 287 seconds. MTOW [lbs] = 132.52 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 = 20.351 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0273297855127176e-12. Allowing negative dual variable(s) as small as -1.107122793183996e-12. Allowing negative dual variable(s) as small as -2.4832777023630637e-12. Allowing negative dual variable(s) as small as -2.482111002073339e-12. Solving took 4 GP solves and 102 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 52.6 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328 MTOW [lbs] = 132.52 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 = 20.351 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0271390229925875e-12. Allowing negative dual variable(s) as small as -1.1071644457479359e-12. Allowing negative dual variable(s) as small as -2.4832202114708416e-12. Allowing negative dual variable(s) as small as -2.482010985584289e-12. Solving took 4 GP solves and 63.9 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 32.9 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328