Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171110150343)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.2713571515e-13. Allowing negative dual variable(s) as small as -2.76185758291e-13. Solving took 4 GP solves and 1.28 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.26061487637e-13. Allowing negative dual variable(s) as small as -2.81152271603e-13. Solving took 4 GP solves and 1.28 seconds. Allowing negative dual variable(s) as small as -2.37062886682e-12. Allowing negative dual variable(s) as small as -2.69888278392e-13. Allowing negative dual variable(s) as small as -1.09859528159e-12. Allowing negative dual variable(s) as small as -1.10446591109e-12. Allowing negative dual variable(s) as small as -1.0976745771e-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 -2.20892683485e-12. Allowing negative dual variable(s) as small as -7.06833680128e-14. Allowing negative dual variable(s) as small as -1.181576538e-13. Allowing negative dual variable(s) as small as -1.18523029932e-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 -1.01246033897e-13. Allowing negative dual variable(s) as small as -2.05757677035e-12. Allowing negative dual variable(s) as small as -2.07824392179e-12. Solving took 4 GP solves and 1.69 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.18511145878e-12. Solving took 4 GP solves and 1.06 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -2.37233583472e-12. Allowing negative dual variable(s) as small as -2.70529258717e-13. Allowing negative dual variable(s) as small as -1.09715079903e-12. Allowing negative dual variable(s) as small as -1.1052822069e-12. Allowing negative dual variable(s) as small as -1.09652207019e-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 -2.2106383564e-12. Allowing negative dual variable(s) as small as -6.94448838712e-14. Allowing negative dual variable(s) as small as -1.18585154717e-13. Allowing negative dual variable(s) as small as -1.17609481182e-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 -1.02734565924e-13. Allowing negative dual variable(s) as small as -2.06251365498e-12. Allowing negative dual variable(s) as small as -2.0764222057e-12. Solving took 4 GP solves and 1.81 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.18219972542e-12. Solving took 4 GP solves and 1.21 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012