Integrated Guidance and Control of Homing Missiles Against Ground Fixed Targets

• Published in: Chinese journal of aeronautics Vol. 21; no. 2; pp. 162 - 168
• Main Authors: Mingzhe, Hou, Guangren, Duan
• Format: Journal Article
• Language: English
• Published: Elsevier Ltd 01.04.2008; Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China
• Subjects: adaptive; ground fixed target; integrated guidance and control; nonlinear; pitch plane; 地面固定目标; 导航系统; 投掷飞机; 自控导弹; pitch plane; ground fixed target; adaptive; nonlinear; integrated guidance and control
• ISSN: 1000-9361
• DOI: 10.1016/S1000-9361(08)60021-7

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.