Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180428145015)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.219739571127313e-14. Allowing negative dual variable(s) as small as -7.455277714618624e-14. Allowing negative dual variable(s) as small as -1.5124143257216893e-13. Allowing negative dual variable(s) as small as -1.5034197844987496e-13. Solving took 4 GP solves and 1.49 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -4.976791548316761e-14. Allowing negative dual variable(s) as small as -7.349589686844737e-14. Allowing negative dual variable(s) as small as -1.4906565565242502e-13. Allowing negative dual variable(s) as small as -1.4885445306922485e-13. Solving took 4 GP solves and 2.66 seconds. Allowing negative dual variable(s) as small as -5.188054846838597e-13. Allowing negative dual variable(s) as small as -1.4305084894417064e-12. Allowing negative dual variable(s) as small as -4.443008461141318e-13. Allowing negative dual variable(s) as small as -4.433640954371043e-13. Allowing negative dual variable(s) as small as -1.2970375641574439e-12. Allowing negative dual variable(s) as small as -1.090706301318245e-12. Allowing negative dual variable(s) as small as -1.0900240128910998e-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 -2.4208442189884924e-14. Allowing negative dual variable(s) as small as -5.696078658777511e-12. Allowing negative dual variable(s) as small as -2.087891440169102e-11. Allowing negative dual variable(s) as small as -2.088077509249231e-11. Solving took 4 GP solves and 1.85 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.79 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.176553630192871e-13. Allowing negative dual variable(s) as small as -1.4304200185444316e-12. Allowing negative dual variable(s) as small as -4.4475187421788576e-13. Allowing negative dual variable(s) as small as -4.4558107203940267e-13. Allowing negative dual variable(s) as small as -1.296803376488187e-12. Allowing negative dual variable(s) as small as -1.0926626357182778e-12. Allowing negative dual variable(s) as small as -1.0907542230542688e-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 -2.497929712314879e-14. Allowing negative dual variable(s) as small as -5.696092591887158e-12. Allowing negative dual variable(s) as small as -2.0879010539454076e-11. Allowing negative dual variable(s) as small as -2.0881047093512277e-11. Solving took 4 GP solves and 2.07 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.48 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417