Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180111113842)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.8665589867082897e-13. Allowing negative dual variable(s) as small as -5.070882949653743e-13. Allowing negative dual variable(s) as small as -1.1294025610564251e-13. Allowing negative dual variable(s) as small as -1.170476476158866e-13. Solving took 4 GP solves and 2.75 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -3.0070303885798566e-13. Allowing negative dual variable(s) as small as -5.126912349523449e-13. Allowing negative dual variable(s) as small as -9.81237660568901e-14. Allowing negative dual variable(s) as small as -1.1988392049910868e-13. Solving took 4 GP solves and 2.75 seconds. MTOW [lbs] = 132.52 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 = 20.351 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.027353962519715e-12. Allowing negative dual variable(s) as small as -1.1070982176810843e-12. Allowing negative dual variable(s) as small as -2.483316863685646e-12. Allowing negative dual variable(s) as small as -2.4820605596863782e-12. Solving took 4 GP solves and 2.43 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 2.25 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328 MTOW [lbs] = 132.52 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 = 20.351 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.299 optimum loiter speed for min power, start of loiter [m/s] = 23.617 optimum loiter speed for min power, end of loiter [m/s] = 16.684 optimum cruise speed, inbound [m/s] = 31.019 optimum cruise speed, outbound [m/s] = 23.408 Beginning signomial solve. Allowing negative dual variable(s) as small as -5.027316089439947e-12. Allowing negative dual variable(s) as small as -1.107254737297863e-12. Allowing negative dual variable(s) as small as -2.483296450163493e-12. Allowing negative dual variable(s) as small as -2.4820923255676068e-12. Solving took 4 GP solves and 2.71 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 1.85 seconds. Max payload weight [lbf] = 9.202 Max take off weight [lbf] = 140.328