Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171104135843)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.13424027115e-13. Allowing negative dual variable(s) as small as -7.00881193361e-13. Solving took 4 GP solves and 1.21 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.13424027115e-13. Allowing negative dual variable(s) as small as -7.00881193361e-13. Solving took 4 GP solves and 1.01 seconds. Allowing negative dual variable(s) as small as -2.37041896528e-12. Allowing negative dual variable(s) as small as -2.71481838746e-13. Allowing negative dual variable(s) as small as -1.0965677151e-12. Allowing negative dual variable(s) as small as -1.1049180234e-12. Allowing negative dual variable(s) as small as -1.09640085639e-12. MTOW [lbs] = 141.59 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 = 21.754 speed at top of climb [m/s] = 26.532 design loiter speed [m/s] = 25.052 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.21014916438e-12. Allowing negative dual variable(s) as small as -7.06454209368e-14. Allowing negative dual variable(s) as small as -1.18886996602e-13. Allowing negative dual variable(s) as small as -1.17911214646e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.190 optimum loiter speed for min power, end of loiter [m/s] = 17.170 optimum cruise speed, inbound [m/s] = 35.882 optimum cruise speed, outbound [m/s] = 25.488 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.01295510627e-13. Allowing negative dual variable(s) as small as -2.06011842559e-12. Allowing negative dual variable(s) as small as -2.07832074122e-12. Solving took 4 GP solves and 2.18 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.18209564201e-12. Solving took 4 GP solves and 1.81 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -2.37041896528e-12. Allowing negative dual variable(s) as small as -2.71481838746e-13. Allowing negative dual variable(s) as small as -1.0965677151e-12. Allowing negative dual variable(s) as small as -1.1049180234e-12. Allowing negative dual variable(s) as small as -1.09640085639e-12. MTOW [lbs] = 141.59 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 = 21.754 speed at top of climb [m/s] = 26.532 design loiter speed [m/s] = 25.052 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.21014916438e-12. Allowing negative dual variable(s) as small as -7.06454209368e-14. Allowing negative dual variable(s) as small as -1.18886996602e-13. Allowing negative dual variable(s) as small as -1.17911214646e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.190 optimum loiter speed for min power, end of loiter [m/s] = 17.170 optimum cruise speed, inbound [m/s] = 35.882 optimum cruise speed, outbound [m/s] = 25.488 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.01295510627e-13. Allowing negative dual variable(s) as small as -2.06011842559e-12. Allowing negative dual variable(s) as small as -2.07832074122e-12. Solving took 4 GP solves and 2.34 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.18209564201e-12. Solving took 4 GP solves and 1.15 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012