Integrated Guidance and Control of Homing Missiles Against Ground Fixed Targets

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• 作者：Hou Mingzhe ; Duan Guangren
• 关键词：integrated guidance and control ; pitch plane ; ground fixed target ; nonlinear ; adaptive
• 刊名：Chinese Journal of Aeronautics
• 出版年：2008
• 出版时间：April 2008
• 年：2008
• 卷：21
• 期：2
• 页码：162-168
• 全文大小：216 K

文摘

This paper presents a scheme of integrated guidance and autopilot design for homing missiles against ground fixed targets. An integrated guidance and control model in the pitch plane is formulated and further changed into a normal form by nonlinear coordinate transformation. By adopting the sliding mode control approach, an adaptive nonlinear control law of the system is designed so that the missile can hit the target accurately with a desired impact attitude angle. The stability analysis of the closed-loop system is also conducted. The numerical simulation has confirmed the usefulness of the proposed design scheme.