| 攻击地面固定目标寻的导弹的一体化制导与控制(英文) |
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| 作者单位： | 哈尔滨工业大学控制理论与制导技术研究中心，哈尔滨工业大学控制理论与制导技术研究中心 黑龙江哈尔滨 150001，黑龙江哈尔滨 150001 |
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| 基金项目： | Major Program of National Natural Science Founda- tion of China (60710002); Program for Changjiang Scholars and Innovative Research Team in Umversity |
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| 摘 要： | 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.
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| 关 键 词： | 投掷飞机 地面固定目标 自控导弹 导航系统 |
| 收稿时间： | 2007-10-19 |
Integrated Guidance and Control of Homing Missiles Against Ground Fixed Targets |
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| Hou ,Duan ,. Integrated Guidance and Control of Homing Missiles Against Ground Fixed Targets[J]. Chinese Journal of Aeronautics, 2008, 21(2): 162-168. DOI: 10.1016/S1000-9361(08)60021-7 |
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| Authors: | Hou Duan |
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| Affiliation: | Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China |
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| Abstract: | This paper presents a scheme of integrated guidance and autopilot design for homing missiles against ground fixed targets. An in- tegrated 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 con- ducted. The numerical simulation has confirmed the usefulness of the proposed design scheme. |
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| Keywords: | integrated guidance and control pitch plane ground fixed target nonlinear adaptive |
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