Abstract
Integrated guidance and control for homing missiles utilizing adaptive dynamic surface control approach is considered based on the three channels independence design idea. A time-varying integrated guidance and control model with unmatched uncertainties is first formulated for the pitch channel, and an adaptive dynamic surface control algorithm is further developed to deal with these unmatched uncertainties. It is proved that the proposed feedback controller can ensure not only the accuracy of target interception, but also the stability of the missile dynamics. Then, the same control approach is further applied to the control design of the yaw and roll channels. The 6-degree-of-freedom (6-DOF) nonlinear missile simulation results demonstrate the feasibility and advantage of the proposed integrated guidance and control design scheme.
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This work was supported by National Natural Science Foundation of China (No. 60710002, No. 60974044).
Ming-Zhe Hou received his B. Eng. degree in automation in 2005 from Harbin Institute of Technology, PRC. Now, he is a Ph. D. candidate in the Center for Control Theory and Guidance Technology at Harbin Institute of Technology.
His research interests include nonlinear control theory and integrated guidance and control for aircrafts.
Guang-Ren Duan received the Ph.D. degree in control systems theory from Harbin Institute of Technology, PRC in 1989. From 1989 to 1991, he was a postdoctoral researcher at Harbin Institute of Technology, where he became a professor of control systems theory in 1991. He visited the University of Hull, UK, and the University of Sheffield, UK from December 1996 to October 1998, and worked at the Queen’s University of Belfast, UK from October 1998 to October 2002. Since August 2000, he has been elected Specially Employed Professor at Harbin Institute of Technology sponsored by the Cheung Kong Scholars Program of the Chinese government. He is currently the director of the Center for Control Systems and Guidance Technology at Harbin Institute of Technology. He is a chartered engineer in the UK, a senior member of IEEE, and a fellow of IEE.
His research interests include robust control, eigenstructure assignment, descriptor systems, missile autopilot design, and magnetic bearing control.
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Hou, MZ., Duan, GR. Adaptive dynamic surface control for integrated missile guidance and autopilot. Int. J. Autom. Comput. 8, 122–127 (2011). https://doi.org/10.1007/s11633-010-0563-z
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DOI: https://doi.org/10.1007/s11633-010-0563-z