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Roll-Pitch-Yaw Integrated H Controller Synthesis for High Angle-of-Attack Missiles
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 Title & Authors
Roll-Pitch-Yaw Integrated H Controller Synthesis for High Angle-of-Attack Missiles
Choi, Byung-Hun; Kang, Seon-Hyeok; Kim, H. Jin; Won, Dae-Yeon; Kim, Youn-Hwan; Jun, Byung-Eul; Lee, Jin-Ik;
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 Abstract
In this work, we explore the feasibility of roll-pitch-yaw integrated autopilots for high angle-of-attack missiles. An investigation of the aerodynamic characteristics of a surface-to-air missile is presented, which reveals the strong effects of cross coupling between the longitudinal and lateral dynamics. Robust control techniques based on H∞ synthesis are employed to design roll-pitch-yaw integrated autopilots. The performance of the proposed roll-pitch-yaw integrated controller is tested in high-fidelity nonlinear five-degree-of-freedom simulations accounting for kinematic cross-coupling effects between the lateral and longitudinal channels. Against nonlinearity and cross-coupling effects of the missile dynamics, the integrated controller demonstrates superior performance when compared with the controller designed in a decoupled manner.
 Keywords
Autopilot;High angle-of-attack missile;Robust control;
 Language
English
 Cited by
1.
Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H2/H Control,;;;

International Journal of Aeronautical and Space Sciences, 2010. vol.11. 2, pp.131-135 crossref(new window)
1.
Three-Axis Autopilot Design for a High Angle-Of-Attack Missile Using Mixed H2/H∞Control, International Journal of Aeronautical and Space Sciences, 2010, 11, 2, 131  crossref(new windwow)
 References
1.
Dahlgren, J., 2002, 'Robust nonlinear control design for a missile using backstepping', Master's thesis, Linkoping Univ

2.
Jeon, B. and Lee, J., 2007, 'Missile Autopilot Design Based on 5-DOF Models', Proceeding of the KSAS Fall Conference, Cheju, pp. 1109-1112

3.
Friang, J., Duc, G. and Bonnet, J., 1998, 'Robust autopilot for a flexible missile: Loop-shaping H_$\infty$ design and real $\mu$-analysis', J. of Robust and nonlinear Control, Vol. 8, pp. 129-153 crossref(new window)

4.
Buschek, H., 1999, 'Full Envelop Missile Autopilot Design using Gain Scheduled Robust Control', J. of Guidance, Control, and Dynamics, Vol. 22, No. 1

5.
Carter, L. and Shamma, J,. 1996, 'Gain-Scheduled Bank-to-Turn Autopilot Design Using Linear Parameter Varying Transformation', J. of Guidance, Control, and Dynamics, Vol. 19, No. 5

6.
Skogestad, S. and Postlethwaite, I., 2003, Multivariable feedback control, John Wiley & Sons, New York

7.
Doyle, J. C. and Zbou, K., 1998, Essential of robust control, Prentice Hall, New Jersey

8.
Lin, C. F., Clutier, J. R. and Evers J. H. 1995, 'Robust Bank-to-Turn Missile Autopilot Design', Proceeding of the American Control Conference, Seattle, pp. 1941-1945

9.
Hull, R. A., 1995, 'Design and Evaluation of Robust Nonlinear Missile Autopilots from a Performance Perspective', Proceeding of the American Control Conference, Seattle, pp. 189-193