Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20180110083840)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.652383521151158e-13. Allowing negative dual variable(s) as small as -4.4698858329972335e-13. Allowing negative dual variable(s) as small as -7.988271502612498e-14. Allowing negative dual variable(s) as small as -9.648206712731255e-14. Solving took 4 GP solves and 4.9 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.6471836875319177e-13. Allowing negative dual variable(s) as small as -4.715151880052559e-13. Allowing negative dual variable(s) as small as -1.030976519433846e-13. Allowing negative dual variable(s) as small as -7.552660753751272e-14. Solving took 4 GP solves and 169 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 -5.027305037962856e-12. Allowing negative dual variable(s) as small as -1.1071728783066873e-12. Allowing negative dual variable(s) as small as -2.483316467476059e-12. Allowing negative dual variable(s) as small as -2.4819337837556194e-12. Solving took 4 GP solves and 50.2 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.82 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 -5.027275898772156e-12. Allowing negative dual variable(s) as small as -1.1070943224826167e-12. Allowing negative dual variable(s) as small as -2.483370274011534e-12. Allowing negative dual variable(s) as small as -2.481984975278702e-12. Solving took 4 GP solves and 4.27 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 14.6 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328