Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180428095323)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -4.962176503031657e-14. Allowing negative dual variable(s) as small as -7.66951606390176e-14. Allowing negative dual variable(s) as small as -1.5117204363312986e-13. Allowing negative dual variable(s) as small as -1.4655160765486563e-13. Solving took 4 GP solves and 3.7 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.1811853418737286e-14. Allowing negative dual variable(s) as small as -7.373095189944223e-14. Allowing negative dual variable(s) as small as -1.4907693135501887e-13. Allowing negative dual variable(s) as small as -1.4826855021521368e-13. Solving took 4 GP solves and 3.28 seconds. Allowing negative dual variable(s) as small as -5.18106391123041e-13. Allowing negative dual variable(s) as small as -1.431054927336639e-12. Allowing negative dual variable(s) as small as -4.4566607348972553e-13. Allowing negative dual variable(s) as small as -4.4441533786354626e-13. Allowing negative dual variable(s) as small as -1.2968578034372458e-12. Allowing negative dual variable(s) as small as -1.092011897574352e-12. Allowing negative dual variable(s) as small as -1.0902651394542606e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 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 = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.479799088545931e-14. Allowing negative dual variable(s) as small as -5.696020621668152e-12. Allowing negative dual variable(s) as small as -2.0879005876378883e-11. Allowing negative dual variable(s) as small as -2.088085500917738e-11. Solving took 4 GP solves and 2.99 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.29 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.17207804362485e-13. Allowing negative dual variable(s) as small as -1.429646331874146e-12. Allowing negative dual variable(s) as small as -4.4589679171203045e-13. Allowing negative dual variable(s) as small as -4.4656292552680554e-13. Allowing negative dual variable(s) as small as -1.2979047090549978e-12. Allowing negative dual variable(s) as small as -1.090401857348211e-12. Allowing negative dual variable(s) as small as -1.0910458734386674e-12. MTOW [lbs] = 141.77 Zero fuel weight [lbs] = 53.80 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 = 21.829 speed at top of climb [m/s] = 26.622 design loiter speed [m/s] = 25.070 rotation speed at 55 lbs [m/s] = 18.185 rotation speed at 150 lbs [m/s] = 28.236 Allowing negative dual variable(s) as small as -1.3717325886286602e-15. optimum loiter speed for min power, start of loiter [m/s] = 25.279 optimum loiter speed for min power, end of loiter [m/s] = 17.233 optimum cruise speed, inbound [m/s] = 36.269 optimum cruise speed, outbound [m/s] = 25.637 Beginning signomial solve. Allowing negative dual variable(s) as small as -2.404943557683957e-14. Allowing negative dual variable(s) as small as -5.696003693899989e-12. Allowing negative dual variable(s) as small as -2.087902899352267e-11. Allowing negative dual variable(s) as small as -2.0880681265435133e-11. Solving took 4 GP solves and 3.42 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 2.94 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417