Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20180328102030)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -8.08212004266e-14. Allowing negative dual variable(s) as small as -8.04872661575e-14. Allowing negative dual variable(s) as small as -1.50118199121e-13. Allowing negative dual variable(s) as small as -1.4885488675e-13. Solving took 4 GP solves and 63.2 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -8.01134332484e-14. Allowing negative dual variable(s) as small as -8.0075269332e-14. Allowing negative dual variable(s) as small as -1.52616634608e-13. Allowing negative dual variable(s) as small as -1.48730854022e-13. Solving took 4 GP solves and 20 seconds. Allowing negative dual variable(s) as small as -5.23194335078e-13. Allowing negative dual variable(s) as small as -5.13186715345e-13. Allowing negative dual variable(s) as small as -5.1527532241e-13. Allowing negative dual variable(s) as small as -5.16789736005e-13. Allowing negative dual variable(s) as small as -2.33797356475e-13. Allowing negative dual variable(s) as small as -1.87084505873e-14. Allowing negative dual variable(s) as small as -1.25964516595e-12. Allowing negative dual variable(s) as small as -1.25995329621e-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 -1.54702639588e-14. Allowing negative dual variable(s) as small as -1.15198866071e-13. 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 -5.43412102115e-11. Allowing negative dual variable(s) as small as -6.4496174801e-12. Allowing negative dual variable(s) as small as -1.93391138073e-11. Allowing negative dual variable(s) as small as -1.9354643913e-11. Solving took 4 GP solves and 23.1 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 9.44 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.23471890834e-13. Allowing negative dual variable(s) as small as -5.12648951068e-13. Allowing negative dual variable(s) as small as -5.13681111536e-13. Allowing negative dual variable(s) as small as -5.16520853866e-13. Allowing negative dual variable(s) as small as -2.36490514671e-13. Allowing negative dual variable(s) as small as -1.94156756644e-14. Allowing negative dual variable(s) as small as -1.26023659824e-12. Allowing negative dual variable(s) as small as -1.25874918128e-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 -1.81564832613e-14. Allowing negative dual variable(s) as small as -1.1343139969e-13. 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 -5.43412621953e-11. Allowing negative dual variable(s) as small as -6.44948819275e-12. Allowing negative dual variable(s) as small as -1.93392508401e-11. Allowing negative dual variable(s) as small as -1.93545675039e-11. Solving took 4 GP solves and 13.7 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 9.06 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417