Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_conif (from gpkit.tests.from_paths.TestFiles-20200214163241)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -1.3139055815569733e-13. Solving took 4 GP solves and 1.85 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -1.28414e-13. Solving took 4 GP solves and 1.95 seconds. Beginning signomial solve. Solving took 4 GP solves and 1.77 seconds. Allowing negative dual variable(s) as small as -1.0243542125643046e-12. Allowing negative dual variable(s) as small as -1.1156442523280186e-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] = 25.637 optimum cruise speed, outbound [m/s] = 36.269 Beginning signomial solve. Allowing negative dual variable(s) as small as -6.468698476891533e-12. Solving took 4 GP solves and 2.37 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.56 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -1.021897e-12. Allowing negative dual variable(s) as small as -1.114867e-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] = 25.637 optimum cruise speed, outbound [m/s] = 36.269 Beginning signomial solve. Allowing negative dual variable(s) as small as -6.468857e-12. Solving took 4 GP solves and 2.45 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.56 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.418 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] = 25.637 optimum cruise speed, outbound [m/s] = 36.269 Beginning signomial solve. Solving took 4 GP solves and 2.53 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 1.93 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.418
Standard Error
/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/venv2_gpkit/local/lib/python2.7/site-packages/pint/quantity.py:1377: UnitStrippedWarning: The unit of the quantity is stripped. warnings.warn("The unit of the quantity is stripped.", UnitStrippedWarning)