Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171205104613)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -8.91819821117e-13. Allowing negative dual variable(s) as small as -4.94759832062e-13. Allowing negative dual variable(s) as small as -1.34026687318e-12. Allowing negative dual variable(s) as small as -1.35732267439e-12. Solving took 4 GP solves and 4.88 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -8.03807975042e-13. Allowing negative dual variable(s) as small as -6.44699354665e-13. Allowing negative dual variable(s) as small as -1.17824673629e-12. Allowing negative dual variable(s) as small as -1.13646743925e-12. Solving took 4 GP solves and 8.61 seconds. Allowing negative dual variable(s) as small as -9.54648686491e-14. Allowing negative dual variable(s) as small as -7.33067361154e-13. Allowing negative dual variable(s) as small as -7.31781497378e-13. Allowing negative dual variable(s) as small as -5.95630999031e-10. Allowing negative dual variable(s) as small as -4.83015293344e-13. Allowing negative dual variable(s) as small as -3.70078859051e-14. MTOW [lbs] = 132.53 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 = 20.352 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.301 Allowing negative dual variable(s) as small as -2.358063831e-14. optimum loiter speed for min power, start of loiter [m/s] = 23.618 optimum loiter speed for min power, end of loiter [m/s] = 16.685 optimum cruise speed, inbound [m/s] = 31.024 optimum cruise speed, outbound [m/s] = 23.411 Beginning signomial solve. Allowing negative dual variable(s) as small as -8.88431333242e-12. Allowing negative dual variable(s) as small as -2.87606582975e-12. Allowing negative dual variable(s) as small as -4.72567622419e-12. Allowing negative dual variable(s) as small as -4.72774269559e-12. Solving took 4 GP solves and 46.3 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 29.3 seconds. Max payload weight [lbf] = 9.228 Max take off weight [lbf] = 140.364 Allowing negative dual variable(s) as small as -9.62846339117e-14. Allowing negative dual variable(s) as small as -7.34551850769e-13. Allowing negative dual variable(s) as small as -7.33885608534e-13. Allowing negative dual variable(s) as small as -5.95630344363e-10. Allowing negative dual variable(s) as small as -4.84961842819e-13. Allowing negative dual variable(s) as small as -3.58775780352e-14. MTOW [lbs] = 132.53 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 = 20.352 speed at top of climb [m/s] = 25.000 design loiter speed [m/s] = 25.000 rotation speed at 55 lbs [m/s] = 18.158 rotation speed at 150 lbs [m/s] = 27.301 Allowing negative dual variable(s) as small as -2.11687492622e-14. optimum loiter speed for min power, start of loiter [m/s] = 23.618 optimum loiter speed for min power, end of loiter [m/s] = 16.685 optimum cruise speed, inbound [m/s] = 31.024 optimum cruise speed, outbound [m/s] = 23.411 Beginning signomial solve. Allowing negative dual variable(s) as small as -8.88445930509e-12. Allowing negative dual variable(s) as small as -2.8760482487e-12. Allowing negative dual variable(s) as small as -4.72558463793e-12. Allowing negative dual variable(s) as small as -4.72775367157e-12. Solving took 4 GP solves and 5.19 seconds. Max Speed [m/s]: 64.61 Beginning signomial solve. Solving took 4 GP solves and 9.31 seconds. Max payload weight [lbf] = 9.228 Max take off weight [lbf] = 140.364