Passed
gpkit.tests.from_paths.TestFiles.test_model_print_perf_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018110753)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -9.82109359116e-14. Allowing negative dual variable(s) as small as -1.20098766002e-12. Allowing negative dual variable(s) as small as -1.13344533412e-12. Allowing negative dual variable(s) as small as -1.13336727156e-12. Solving took 4 GP solves and 2.23 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -9.83774693653e-14. Allowing negative dual variable(s) as small as -1.18665103785e-12. Allowing negative dual variable(s) as small as -1.13640520605e-12. Allowing negative dual variable(s) as small as -1.1256091545e-12. Solving took 4 GP solves and 2.05 seconds. Allowing negative dual variable(s) as small as -1.56935575646e-12. Allowing negative dual variable(s) as small as -3.9607648758e-12. Allowing negative dual variable(s) as small as -1.78750157037e-12. Allowing negative dual variable(s) as small as -2.08239848976e-12. Allowing negative dual variable(s) as small as -2.08095606719e-12. Allowing negative dual variable(s) as small as -4.73684026031e-13. Allowing negative dual variable(s) as small as -8.92673088226e-13. Allowing negative dual variable(s) as small as -9.40558178217e-13. Allowing negative dual variable(s) as small as -9.43293620298e-13. 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 = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 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 -2.38523176904e-13. Allowing negative dual variable(s) as small as -9.1885049916e-14. Allowing negative dual variable(s) as small as -1.2078760301e-13. Allowing negative dual variable(s) as small as -1.1972454278e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.6098190398e-13. Allowing negative dual variable(s) as small as -2.0170853723e-12. Allowing negative dual variable(s) as small as -1.23793879006e-14. Allowing negative dual variable(s) as small as -1.70982214728e-14. Solving took 4 GP solves and 2.75 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 1.79 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -1.56958213787e-12. Allowing negative dual variable(s) as small as -3.9605246166e-12. Allowing negative dual variable(s) as small as -1.78657783012e-12. Allowing negative dual variable(s) as small as -2.08217731251e-12. Allowing negative dual variable(s) as small as -2.08069585866e-12. Allowing negative dual variable(s) as small as -4.71395708926e-13. Allowing negative dual variable(s) as small as -8.93394950033e-13. Allowing negative dual variable(s) as small as -9.42780033729e-13. Allowing negative dual variable(s) as small as -9.42525246218e-13. 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 = 21.712 speed at top of climb [m/s] = 26.507 design loiter speed [m/s] = 25.048 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 -2.31551323254e-13. Allowing negative dual variable(s) as small as -9.29851898604e-14. Allowing negative dual variable(s) as small as -1.18552411811e-13. Allowing negative dual variable(s) as small as -1.21156665429e-13. optimum loiter speed for min power, start of loiter [m/s] = 25.166 optimum loiter speed for min power, end of loiter [m/s] = 17.158 optimum cruise speed, inbound [m/s] = 35.697 optimum cruise speed, outbound [m/s] = 25.443 Beginning signomial solve. Allowing negative dual variable(s) as small as -9.62081417544e-13. Allowing negative dual variable(s) as small as -2.01675802604e-12. Allowing negative dual variable(s) as small as -1.23215023042e-14. Allowing negative dual variable(s) as small as -1.76472020019e-14. Solving took 4 GP solves and 3.15 seconds. Warning: Variable [Re_Mission/Loiter/FlightSegment.2/AircraftPerf.2/TailAero.5_(0,), Re_Mission/Loiter/FlightSegment.2 could cause inaccurate result because it is above upper bound. Solution is 1021559.0193 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Solving took 4 GP solves and 1.87 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531