Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek (from gpkit.tests.from_paths.TestFiles-20171110174119)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.07913244313e-13. Allowing negative dual variable(s) as small as -1.07412342909e-13. Solving took 4 GP solves and 2.23 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.10777706452e-13. Allowing negative dual variable(s) as small as -1.07869876226e-13. Allowing negative dual variable(s) as small as -2.36356073602e-16. Solving took 4 GP solves and 1.97 seconds. Allowing negative dual variable(s) as small as -3.88100662718e-12. Allowing negative dual variable(s) as small as -1.7118364018e-12. Allowing negative dual variable(s) as small as -7.74809903736e-13. Allowing negative dual variable(s) as small as -7.70186865673e-13. Allowing negative dual variable(s) as small as -7.70372481085e-13. Allowing negative dual variable(s) as small as -2.46703915976e-13. Allowing negative dual variable(s) as small as -1.01880461532e-12. Allowing negative dual variable(s) as small as -1.05903155169e-12. Allowing negative dual variable(s) as small as -1.04737225837e-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 -2.59041919859e-13. Allowing negative dual variable(s) as small as -1.47748024752e-13. Allowing negative dual variable(s) as small as -1.44109333841e-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 -4.00610677054e-13. Allowing negative dual variable(s) as small as -2.22259841291e-15. Allowing negative dual variable(s) as small as -9.04018729907e-14. Allowing negative dual variable(s) as small as -8.97778470366e-14. Solving took 4 GP solves and 2.69 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Solving took 4 GP solves and 1.74 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -3.88050355737e-12. Allowing negative dual variable(s) as small as -1.71231778756e-12. Allowing negative dual variable(s) as small as -7.75299095757e-13. Allowing negative dual variable(s) as small as -7.70548555518e-13. Allowing negative dual variable(s) as small as -7.6976619523e-13. Allowing negative dual variable(s) as small as -2.49025409668e-13. Allowing negative dual variable(s) as small as -1.0177963073e-12. Allowing negative dual variable(s) as small as -1.05662787547e-12. Allowing negative dual variable(s) as small as -1.04758454515e-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 -2.58987276069e-13. Allowing negative dual variable(s) as small as -1.46784602702e-13. Allowing negative dual variable(s) as small as -1.47001768397e-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 -4.0009461122e-13. Allowing negative dual variable(s) as small as -4.12699328201e-15. Allowing negative dual variable(s) as small as -8.72982324107e-14. Allowing negative dual variable(s) as small as -8.94190805673e-14. Solving took 4 GP solves and 2.73 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Solving took 4 GP solves and 1.72 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012