Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171031162642)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -3.71845913436e-12. Allowing negative dual variable(s) as small as -1.87220633961e-11. Allowing negative dual variable(s) as small as -3.62182072527e-13. Allowing negative dual variable(s) as small as -4.61109015554e-13. Solving took 4 GP solves and 3.44 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -3.71845913436e-12. Allowing negative dual variable(s) as small as -1.87220633961e-11. Allowing negative dual variable(s) as small as -3.62182072527e-13. Allowing negative dual variable(s) as small as -4.61109015554e-13. Solving took 4 GP solves and 2.75 seconds. Allowing negative dual variable(s) as small as -2.31380123394e-11. Allowing negative dual variable(s) as small as -8.79610967397e-12. Allowing negative dual variable(s) as small as -1.98742064472e-11. Allowing negative dual variable(s) as small as -7.68574787147e-12. Allowing negative dual variable(s) as small as -7.66163521515e-12. Allowing negative dual variable(s) as small as -2.36046358241e-11. Allowing negative dual variable(s) as small as -1.17887586628e-11. Allowing negative dual variable(s) as small as -1.1977331453e-11. Allowing negative dual variable(s) as small as -1.17717234615e-11. MTOW [lbs] = 141.59 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 = 21.754 speed at top of climb [m/s] = 26.532 design loiter speed [m/s] = 25.052 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.73221625446e-11. Allowing negative dual variable(s) as small as -1.24184061472e-11. Allowing negative dual variable(s) as small as -7.11262754423e-12. Allowing negative dual variable(s) as small as -6.64457584006e-12. optimum loiter speed for min power, start of loiter [m/s] = 25.190 optimum loiter speed for min power, end of loiter [m/s] = 17.170 optimum cruise speed, inbound [m/s] = 35.882 optimum cruise speed, outbound [m/s] = 25.488 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.45685117514e-12. Allowing negative dual variable(s) as small as -2.4004082752e-12. Allowing negative dual variable(s) as small as -7.67767478698e-11. Allowing negative dual variable(s) as small as -8.54843495689e-11. Solving took 4 GP solves and 4.28 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.93834314119e-12. Allowing negative dual variable(s) as small as -3.89277473103e-11. Allowing negative dual variable(s) as small as -5.41168030527e-11. Allowing negative dual variable(s) as small as -5.45077355647e-11. Solving took 4 GP solves and 3.42 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012 Allowing negative dual variable(s) as small as -2.31380123394e-11. Allowing negative dual variable(s) as small as -8.79610967397e-12. Allowing negative dual variable(s) as small as -1.98742064472e-11. Allowing negative dual variable(s) as small as -7.68574787147e-12. Allowing negative dual variable(s) as small as -7.66163521515e-12. Allowing negative dual variable(s) as small as -2.36046358241e-11. Allowing negative dual variable(s) as small as -1.17887586628e-11. Allowing negative dual variable(s) as small as -1.1977331453e-11. Allowing negative dual variable(s) as small as -1.17717234615e-11. MTOW [lbs] = 141.59 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 = 21.754 speed at top of climb [m/s] = 26.532 design loiter speed [m/s] = 25.052 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 28.219 Allowing negative dual variable(s) as small as -2.73221625446e-11. Allowing negative dual variable(s) as small as -1.24184061472e-11. Allowing negative dual variable(s) as small as -7.11262754423e-12. Allowing negative dual variable(s) as small as -6.64457584006e-12. optimum loiter speed for min power, start of loiter [m/s] = 25.190 optimum loiter speed for min power, end of loiter [m/s] = 17.170 optimum cruise speed, inbound [m/s] = 35.882 optimum cruise speed, outbound [m/s] = 25.488 Beginning signomial solve. Allowing negative dual variable(s) as small as -1.45685117514e-12. Allowing negative dual variable(s) as small as -2.4004082752e-12. Allowing negative dual variable(s) as small as -7.67767478698e-11. Allowing negative dual variable(s) as small as -8.54843495689e-11. Solving took 4 GP solves and 4.19 seconds. Max Speed [m/s]: 74.36 Beginning signomial solve. Allowing negative dual variable(s) as small as -3.93834314119e-12. Allowing negative dual variable(s) as small as -3.89277473103e-11. Allowing negative dual variable(s) as small as -5.41168030527e-11. Allowing negative dual variable(s) as small as -5.45077355647e-11. Solving took 4 GP solves and 3.76 seconds. Max payload weight [lbf] = 27.204 Max take off weight [lbf] = 165.012