Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428155324)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -4.895216176858952e-14. Allowing negative dual variable(s) as small as -7.59626736512864e-14. Allowing negative dual variable(s) as small as -1.5116770682443992e-13. Allowing negative dual variable(s) as small as -1.488275648553472e-13. Solving took 4 GP solves and 3.02 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.235742395193199e-14. Allowing negative dual variable(s) as small as -7.533687215732776e-14. Allowing negative dual variable(s) as small as -1.5113301235492038e-13. Allowing negative dual variable(s) as small as -1.4954183724658066e-13. Solving took 4 GP solves and 3.09 seconds. Allowing negative dual variable(s) as small as -5.151989945773039e-13. Allowing negative dual variable(s) as small as -1.4268117937143998e-12. Allowing negative dual variable(s) as small as -4.436399164697846e-13. Allowing negative dual variable(s) as small as -4.432912370511133e-13. Allowing negative dual variable(s) as small as -1.297172438907701e-12. Allowing negative dual variable(s) as small as -1.0913055398589777e-12. Allowing negative dual variable(s) as small as -1.091214900557358e-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 -1.2555061157382141e-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] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.4465827656347365e-14. Allowing negative dual variable(s) as small as -5.695962676541277e-12. Allowing negative dual variable(s) as small as -2.0879046328369573e-11. Allowing negative dual variable(s) as small as -2.088077890808457e-11. Solving took 4 GP solves and 3.08 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.96 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.169250444359008e-13. Allowing negative dual variable(s) as small as -1.429184895429536e-12. Allowing negative dual variable(s) as small as -4.437908374121946e-13. Allowing negative dual variable(s) as small as -4.4295123124982183e-13. Allowing negative dual variable(s) as small as -1.2969347817914922e-12. Allowing negative dual variable(s) as small as -1.0901395888426868e-12. Allowing negative dual variable(s) as small as -1.0907505367668824e-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] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.477564086235482e-14. Allowing negative dual variable(s) as small as -5.696072412835967e-12. Allowing negative dual variable(s) as small as -2.0878930799560664e-11. Allowing negative dual variable(s) as small as -2.0880808627638422e-11. Solving took 4 GP solves and 2.9 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.35 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417