Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171109134712)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.22068154196e-13. Allowing negative dual variable(s) as small as -3.83395572234e-13. Solving took 4 GP solves and 2.67 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.22068154196e-13. Allowing negative dual variable(s) as small as -3.83395572234e-13. Solving took 4 GP solves and 2.43 seconds. Allowing negative dual variable(s) as small as -2.37130540898e-12. Allowing negative dual variable(s) as small as -2.75495338348e-13. Allowing negative dual variable(s) as small as -1.09769658641e-12. Allowing negative dual variable(s) as small as -1.10487714897e-12. Allowing negative dual variable(s) as small as -1.09686023285e-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 -2.21143979864e-12. Allowing negative dual variable(s) as small as -7.1073247114e-14. Allowing negative dual variable(s) as small as -1.18206984999e-13. Allowing negative dual variable(s) as small as -1.17715516154e-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 -1.03061850296e-13. Allowing negative dual variable(s) as small as -2.06082726585e-12. Allowing negative dual variable(s) as small as -2.07713888107e-12. Solving took 4 GP solves and 3.7 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.18493278226e-12. Solving took 4 GP solves and 2.78 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -2.37130540898e-12. Allowing negative dual variable(s) as small as -2.75495338348e-13. Allowing negative dual variable(s) as small as -1.09769658641e-12. Allowing negative dual variable(s) as small as -1.10487714897e-12. Allowing negative dual variable(s) as small as -1.09686023285e-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 -2.21143979864e-12. Allowing negative dual variable(s) as small as -7.1073247114e-14. Allowing negative dual variable(s) as small as -1.18206984999e-13. Allowing negative dual variable(s) as small as -1.17715516154e-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 -1.03061850296e-13. Allowing negative dual variable(s) as small as -2.06082726585e-12. Allowing negative dual variable(s) as small as -2.07713888107e-12. Solving took 4 GP solves and 3.63 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.18493278226e-12. Solving took 4 GP solves and 3 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012