Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20171112202811)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.61036851856e-13. Allowing negative dual variable(s) as small as -9.2916126182e-14. Allowing negative dual variable(s) as small as -2.51369758342e-12. Allowing negative dual variable(s) as small as -2.47040148754e-12. Solving took 4 GP solves and 2.34 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.61036851856e-13. Allowing negative dual variable(s) as small as -9.2916126182e-14. Allowing negative dual variable(s) as small as -2.51369758342e-12. Allowing negative dual variable(s) as small as -2.47040148754e-12. Solving took 4 GP solves and 2.58 seconds. Allowing negative dual variable(s) as small as -3.60041423758e-12. Allowing negative dual variable(s) as small as -1.58857475785e-12. Allowing negative dual variable(s) as small as -1.77729185535e-12. Allowing negative dual variable(s) as small as -7.78800635093e-13. Allowing negative dual variable(s) as small as -7.78106745702e-13. Allowing negative dual variable(s) as small as -2.76403682928e-13. Allowing negative dual variable(s) as small as -1.0992029769e-12. Allowing negative dual variable(s) as small as -1.06869406987e-12. Allowing negative dual variable(s) as small as -1.06195434391e-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 -2.27370596309e-12. Allowing negative dual variable(s) as small as -7.2326367985e-14. Allowing negative dual variable(s) as small as -1.20836825789e-13. Allowing negative dual variable(s) as small as -1.20700433155e-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 -2.64087058162e-12. Allowing negative dual variable(s) as small as -1.98068463003e-12. Allowing negative dual variable(s) as small as -1.9965789459e-12. Solving took 4 GP solves and 2.41 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.85058911839e-12. Solving took 4 GP solves and 1.26 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -3.60041423758e-12. Allowing negative dual variable(s) as small as -1.58857475785e-12. Allowing negative dual variable(s) as small as -1.77729185535e-12. Allowing negative dual variable(s) as small as -7.78800635093e-13. Allowing negative dual variable(s) as small as -7.78106745702e-13. Allowing negative dual variable(s) as small as -2.76403682928e-13. Allowing negative dual variable(s) as small as -1.0992029769e-12. Allowing negative dual variable(s) as small as -1.06869406987e-12. Allowing negative dual variable(s) as small as -1.06195434391e-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 -2.27370596309e-12. Allowing negative dual variable(s) as small as -7.2326367985e-14. Allowing negative dual variable(s) as small as -1.20836825789e-13. Allowing negative dual variable(s) as small as -1.20700433155e-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 -2.64087058162e-12. Allowing negative dual variable(s) as small as -1.98068463003e-12. Allowing negative dual variable(s) as small as -1.9965789459e-12. Solving took 4 GP solves and 2.48 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.85058911839e-12. Solving took 4 GP solves and 1.87 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012