Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171110160237)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.09510924634e-13. Allowing negative dual variable(s) as small as -1.08641828173e-13. Allowing negative dual variable(s) as small as -1.44415729375e-16. Solving took 4 GP solves and 27 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.10319739455e-13. Allowing negative dual variable(s) as small as -1.04542242918e-13. Allowing negative dual variable(s) as small as -1.90385901488e-16. Allowing negative dual variable(s) as small as -1.23165366794e-16. Solving took 4 GP solves and 29.9 seconds. Allowing negative dual variable(s) as small as -3.88104652582e-12. Allowing negative dual variable(s) as small as -1.71179390107e-12. Allowing negative dual variable(s) as small as -7.74775209267e-13. Allowing negative dual variable(s) as small as -7.70266662953e-13. Allowing negative dual variable(s) as small as -7.69832114722e-13. Allowing negative dual variable(s) as small as -2.49261765742e-13. Allowing negative dual variable(s) as small as -1.0145410987e-12. Allowing negative dual variable(s) as small as -1.0579494095e-12. Allowing negative dual variable(s) as small as -1.04745953664e-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 -2.59518968815e-13. Allowing negative dual variable(s) as small as -1.47737833252e-13. Allowing negative dual variable(s) as small as -1.47689260994e-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 -4.00687301984e-13. Allowing negative dual variable(s) as small as -3.41165283517e-17. Allowing negative dual variable(s) as small as -8.5995690873e-14. Allowing negative dual variable(s) as small as -8.95559766029e-14. Solving took 4 GP solves and 18.9 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Solving took 4 GP solves and 20 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -3.8816953124e-12. Allowing negative dual variable(s) as small as -1.71206625266e-12. Allowing negative dual variable(s) as small as -7.75840329481e-13. Allowing negative dual variable(s) as small as -7.70546820794e-13. Allowing negative dual variable(s) as small as -7.70612740286e-13. Allowing negative dual variable(s) as small as -2.51604943477e-13. Allowing negative dual variable(s) as small as -1.01532280847e-12. Allowing negative dual variable(s) as small as -1.05771706498e-12. Allowing negative dual variable(s) as small as -1.04802527334e-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 -2.58537982689e-13. Allowing negative dual variable(s) as small as -1.48172273062e-13. Allowing negative dual variable(s) as small as -1.47868804874e-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 -4.00326085631e-13. Allowing negative dual variable(s) as small as -8.90307958997e-14. Allowing negative dual variable(s) as small as -8.60599474277e-14. Solving took 4 GP solves and 30.8 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Solving took 4 GP solves and 22.9 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012