Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180430090654)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.168001443456305e-14. Allowing negative dual variable(s) as small as -7.66357463599654e-14. Allowing negative dual variable(s) as small as -1.5024570129695825e-13. Allowing negative dual variable(s) as small as -1.5007916784326447e-13. Solving took 4 GP solves and 3 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.063354249768004e-14. Allowing negative dual variable(s) as small as -7.534554577470765e-14. Allowing negative dual variable(s) as small as -1.5139105247197193e-13. Allowing negative dual variable(s) as small as -1.497708207454096e-13. Solving took 4 GP solves and 2.87 seconds. Allowing negative dual variable(s) as small as -5.173760725396548e-13. Allowing negative dual variable(s) as small as -1.4292022426642959e-12. Allowing negative dual variable(s) as small as -4.4327215509287754e-13. Allowing negative dual variable(s) as small as -4.4316807168431893e-13. Allowing negative dual variable(s) as small as -1.2962848025890872e-12. Allowing negative dual variable(s) as small as -1.0908547285956582e-12. Allowing negative dual variable(s) as small as -1.0911237191546519e-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 -2.4995791501609792e-14. Allowing negative dual variable(s) as small as -5.695903911592388e-12. Allowing negative dual variable(s) as small as -2.0878930279350085e-11. Allowing negative dual variable(s) as small as -2.0880859609704485e-11. Solving took 4 GP solves and 2.99 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.07 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.175634226750603e-13. Allowing negative dual variable(s) as small as -1.431353299774507e-12. Allowing negative dual variable(s) as small as -4.440527806570671e-13. Allowing negative dual variable(s) as small as -4.442383960689966e-13. Allowing negative dual variable(s) as small as -1.2969078935776146e-12. Allowing negative dual variable(s) as small as -1.0904344918336029e-12. Allowing negative dual variable(s) as small as -1.0903401662445966e-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 -2.518513449378194e-14. Allowing negative dual variable(s) as small as -5.69591138038481e-12. Allowing negative dual variable(s) as small as -2.087889202329231e-11. Allowing negative dual variable(s) as small as -2.0880829841975633e-11. Solving took 4 GP solves and 2.8 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.94 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417