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Optimal Controller Gain Selection Using the Power Flow Information of Bond Graph Modeling

Optimal Controller Gain Selection Using the Power Flow Information of Bond Graph Modeling. Robert T. McBride Dr. François Cellier Raytheon Missile Systems University of Arizona. Missile System. Fn. θ. α. VM. Two Degree of Freedom Missile. X CPN. X CG. X CPB. X CPW. X HL. L M.

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Optimal Controller Gain Selection Using the Power Flow Information of Bond Graph Modeling

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  1. Optimal Controller Gain Selection Using the Power Flow Information of Bond Graph Modeling Robert T. McBride Dr. François Cellier Raytheon Missile Systems University of Arizona ICBGM'05

  2. Missile System ICBGM'05

  3. Fn θ α VM Two Degree of Freedom Missile ICBGM'05

  4. XCPN XCG XCPB XCPW XHL LM Two DOF Missile: Relative Lengths ICBGM'05

  5. Tip Chord Height Root Chord Wing/Fin Chord Definitions ICBGM'05

  6. Normal Force Equations ICBGM'05

  7. Moment Equations ICBGM'05

  8. Missile Parameters ICBGM'05

  9. Missile System ICBGM'05

  10. Pitch Autopilot/Gain Selection ICBGM'05

  11. 20 G Step Response:Achieved Acceleration ICBGM'05

  12. 20 G Step Response:Achieved Angle of Attack ICBGM'05

  13. 20 G Step Response:Output Energy/Available Energy ICBGM'05

  14. 20 G Step Response:Integral (Output Energy/Available Energy) ICBGM'05

  15. Conclusions • This paper shows, by means of an example of a two-degree of freedom missile simulation, a method, in which a bond-graph actuator model can be used to determine the efficiency of a set of controller gains. • This analysis provides a method for comparing the efficiency of controller gains that can be realized in a quick and affordable manner. ICBGM'05

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