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Passed
gpkit.tests.from_paths.TestFiles.test_model_jho_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20171018105900)
Standard Output
Beginning signomial solve. Allowing negative dual variable(s) as small as -2.07997156824e-11. Allowing negative dual variable(s) as small as -1.60152793804e-12. Allowing negative dual variable(s) as small as -1.69474764083e-12. Allowing negative dual variable(s) as small as -2.24482286058e-11. Solving took 4 GP solves and 1.32 seconds. Beginning signomial solve. Allowing negative dual variable(s) as small as -2.0958317113e-11. Allowing negative dual variable(s) as small as -1.44199669566e-12. Allowing negative dual variable(s) as small as -1.63676537601e-12. Allowing negative dual variable(s) as small as -1.62887498628e-12. Solving took 4 GP solves and 1.24 seconds. Allowing negative dual variable(s) as small as -7.74424274708e-12. Allowing negative dual variable(s) as small as -3.41600706055e-11. Allowing negative dual variable(s) as small as -2.08748643371e-11. Allowing negative dual variable(s) as small as -2.112797437e-11. Allowing negative dual variable(s) as small as -2.13846509944e-11. Allowing negative dual variable(s) as small as -4.88693157122e-12. Allowing negative dual variable(s) as small as -1.04705577975e-11. Allowing negative dual variable(s) as small as -5.89819599411e-12. Allowing negative dual variable(s) as small as -1.10752449963e-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 = 21.712 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 -2.75761705137e-12. Allowing negative dual variable(s) as small as -7.11270950991e-12. Allowing negative dual variable(s) as small as -1.34973838746e-11. Allowing negative dual variable(s) as small as -1.37366241429e-11. 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 -3.42441630667e-11. Allowing negative dual variable(s) as small as -3.57327052526e-11. Allowing negative dual variable(s) as small as -3.97165477056e-13. Allowing negative dual variable(s) as small as -5.6708001202e-11. Solving took 4 GP solves and 1.95 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.01989639492e-13. Allowing negative dual variable(s) as small as -1.8056133845e-11. Allowing negative dual variable(s) as small as -7.28747353261e-11. Allowing negative dual variable(s) as small as -1.43036637222e-11. Solving took 4 GP solves and 1.74 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531 Allowing negative dual variable(s) as small as -7.73682506949e-12. Allowing negative dual variable(s) as small as -3.41888878319e-11. Allowing negative dual variable(s) as small as -2.08928152556e-11. Allowing negative dual variable(s) as small as -2.11521286597e-11. Allowing negative dual variable(s) as small as -2.14118306419e-11. Allowing negative dual variable(s) as small as -4.89125211688e-12. Allowing negative dual variable(s) as small as -1.04706990691e-11. Allowing negative dual variable(s) as small as -5.89447999959e-12. Allowing negative dual variable(s) as small as -1.10742932836e-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 = 21.712 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 -2.78553135419e-12. Allowing negative dual variable(s) as small as -7.11447383211e-12. Allowing negative dual variable(s) as small as -1.34976065698e-11. Allowing negative dual variable(s) as small as -1.37369743402e-11. 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 -3.42467928677e-11. Allowing negative dual variable(s) as small as -3.57339089807e-11. Allowing negative dual variable(s) as small as -3.98204636769e-13. Allowing negative dual variable(s) as small as -5.67072790622e-11. Solving took 4 GP solves and 1.96 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 1021559.0185 but bound is 1000000.0000 Max Speed [m/s]: 73.83 Beginning signomial solve. Allowing negative dual variable(s) as small as -4.07465294144e-13. Allowing negative dual variable(s) as small as -1.80554221747e-11. Allowing negative dual variable(s) as small as -7.28732968067e-11. Allowing negative dual variable(s) as small as -1.42998707493e-11. Solving took 4 GP solves and 2.54 seconds. Max payload weight [lbf] = 26.860 Max take off weight [lbf] = 164.531