The Jenkins Controller is preparing for shutdown. No new builds can be started.
Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek (from gpkit.tests.from_paths.TestFiles-20180424145252)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -5.074803424709451e-14. Allowing negative dual variable(s) as small as -7.32920668600201e-14. Allowing negative dual variable(s) as small as -1.506013196095335e-13. Allowing negative dual variable(s) as small as -1.497933721505973e-13. Solving took 4 GP solves and 7.02 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -5.079573914268387e-14. Allowing negative dual variable(s) as small as -7.106988608729381e-14. Allowing negative dual variable(s) as small as -1.5086066076919202e-13. Allowing negative dual variable(s) as small as -1.488496825796659e-13. Solving took 4 GP solves and 8.33 seconds. Allowing negative dual variable(s) as small as -5.163716676470642e-13. Allowing negative dual variable(s) as small as -1.4297382722183727e-12. Allowing negative dual variable(s) as small as -4.448975909898678e-13. Allowing negative dual variable(s) as small as -4.462732267063174e-13. Allowing negative dual variable(s) as small as -1.2963119076433993e-12. Allowing negative dual variable(s) as small as -1.0908608001278242e-12. Allowing negative dual variable(s) as small as -1.0903739933523782e-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 -2.3902106689400657e-14. Allowing negative dual variable(s) as small as -5.695985459954083e-12. Allowing negative dual variable(s) as small as -2.0878948889193332e-11. Allowing negative dual variable(s) as small as -2.0880758656188545e-11. Solving took 4 GP solves and 8.65 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 3.57 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417 Allowing negative dual variable(s) as small as -5.177646505982736e-13. Allowing negative dual variable(s) as small as -1.4290079536349864e-12. Allowing negative dual variable(s) as small as -4.443060502845597e-13. Allowing negative dual variable(s) as small as -4.437908374121946e-13. Allowing negative dual variable(s) as small as -1.2980563889389285e-12. Allowing negative dual variable(s) as small as -1.0912993599065945e-12. Allowing negative dual variable(s) as small as -1.092105681062272e-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 -2.4368763292185298e-14. Allowing negative dual variable(s) as small as -5.696030617159855e-12. Allowing negative dual variable(s) as small as -2.0879078290601972e-11. Allowing negative dual variable(s) as small as -2.088084711522736e-11. Solving took 4 GP solves and 15.9 seconds. Max Speed [m/s]: 74.76 Beginning signomial solve. Solving took 4 GP solves and 4.04 seconds. Max payload weight [lbf] = 28.083 Max take off weight [lbf] = 166.417