Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180430090758)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.187733922995541e-14. Allowing negative dual variable(s) as small as -7.610275257197152e-14. Allowing negative dual variable(s) as small as -1.5324373714431516e-13. Allowing negative dual variable(s) as small as -1.490530789072242e-13. Solving took 4 GP solves and 1.52 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.1685652285859973e-14. Allowing negative dual variable(s) as small as -7.617387623448657e-14. Allowing negative dual variable(s) as small as -1.5193662300516664e-13. Allowing negative dual variable(s) as small as -1.4918491789139843e-13. Solving took 4 GP solves and 1.56 seconds. Allowing negative dual variable(s) as small as -5.164809552260508e-13. Allowing negative dual variable(s) as small as -1.4290929550853093e-12. Allowing negative dual variable(s) as small as -4.425279587216835e-13. Allowing negative dual variable(s) as small as -4.4369716234449186e-13. Allowing negative dual variable(s) as small as -1.296461419122985e-12. Allowing negative dual variable(s) as small as -1.0906043863140313e-12. Allowing negative dual variable(s) as small as -1.0897607686036204e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 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 = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.3673957799387182e-15. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 25.637 optimum cruise speed, outbound [m/s] = 36.269 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.4224887546314103e-14. Allowing negative dual variable(s) as small as -5.695991936420937e-12. Allowing negative dual variable(s) as small as -2.0878956261953393e-11. Allowing negative dual variable(s) as small as -2.08809198198504e-11. Solving took 4 GP solves and 9.07 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 4.11 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.181636369977483e-13. Allowing negative dual variable(s) as small as -1.4313307483693194e-12. Allowing negative dual variable(s) as small as -4.440527806570671e-13. Allowing negative dual variable(s) as small as -4.4303276325319274e-13. Allowing negative dual variable(s) as small as -1.2955936237041277e-12. Allowing negative dual variable(s) as small as -1.089524195689584e-12. Allowing negative dual variable(s) as small as -1.0905650297751701e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 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 = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 25.637 optimum cruise speed, outbound [m/s] = 36.269 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.452211458387919e-14. Allowing negative dual variable(s) as small as -5.695964096009678e-12. Allowing negative dual variable(s) as small as -2.0878974455241718e-11. Allowing negative dual variable(s) as small as -2.0880738988639375e-11. Solving took 4 GP solves and 1.65 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.3 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417