Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20190417020411)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -4.948689028005937e-14. Allowing negative dual variable(s) as small as -7.08387341841199e-14. Allowing negative dual variable(s) as small as -1.521118300762403e-13. Allowing negative dual variable(s) as small as -1.4869225642422101e-13. Solving took 4 GP solves and 27.1 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.0295705100733556e-14. Allowing negative dual variable(s) as small as -7.45189500384047e-14. Allowing negative dual variable(s) as small as -1.512657187008326e-13. Allowing negative dual variable(s) as small as -1.5031509023599732e-13. Solving took 4 GP solves and 27.1 seconds. Allowing negative dual variable(s) as small as -5.170100458862237e-13. Allowing negative dual variable(s) as small as -1.4284719240809096e-12. Allowing negative dual variable(s) as small as -4.4357746642464946e-13. Allowing negative dual variable(s) as small as -4.4458881021114394e-13. Allowing negative dual variable(s) as small as -1.2975630769504476e-12. Allowing negative dual variable(s) as small as -1.091774132037926e-12. Allowing negative dual variable(s) as small as -1.091371134090413e-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 -3.900959416602845e-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 -2.4382334559945324e-14. Allowing negative dual variable(s) as small as -5.696043392560752e-12. Allowing negative dual variable(s) as small as -2.0879014935449193e-11. Allowing negative dual variable(s) as small as -2.0880786745124565e-11. Solving took 4 GP solves and 20.2 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 12.7 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.186961971048731e-13. Allowing negative dual variable(s) as small as -1.428959381377659e-12. Allowing negative dual variable(s) as small as -4.444188073104982e-13. Allowing negative dual variable(s) as small as -4.4479697702826115e-13. Allowing negative dual variable(s) as small as -1.2967420106452243e-12. Allowing negative dual variable(s) as small as -1.0912951315181219e-12. Allowing negative dual variable(s) as small as -1.0908355382172052e-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 -8.313662258618848e-16. 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 -2.4764022005538215e-14. Allowing negative dual variable(s) as small as -5.695881507782691e-12. Allowing negative dual variable(s) as small as -2.0879003402301523e-11. Allowing negative dual variable(s) as small as -2.0880717878513687e-11. Solving took 4 GP solves and 18.5 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 16.9 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417
Standard Error
/Users/jenkins/workspace/gplibrary_Push_Models/mosek/venv2_gpkit/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)