| 对动态目标制导的导弹动力学逆系统跟踪控制 |
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| 引用本文： | 高坚,许宏,佟明安.对动态目标制导的导弹动力学逆系统跟踪控制[J].飞行力学,2008,26(5). |
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| 作者姓名： | 高坚 许宏 佟明安 |
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| 作者单位： | 1. 中国计量学院,机电工程学院,浙江,杭州,310018
2. 西北工业大学,电子信息学院,陕西,西安,710072 |
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| 基金项目： | 国防预研基金资助项目(4020501) |
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| 摘 要： | 结合目标-导弹的运动特性,运用逆系统方法与制导原理,设计了导弹质心运动的Euler动力学系统跟踪控制器。在控制器设计中,综合考虑了目标飞行状态、控制律、制导律、解耦性及抗干扰性这几个重要因素。通过对弹体坐标系下导弹的外力矩实施控制,实现偏转角速度对动态目标的渐近跟踪控制。通过仿真验证,说明了控制器设计的合理性和有效性。
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| 关 键 词： | 目标特性 Euler方程 逆系统方法 跟踪控制 仿真 |
Tracking Control of Missile's Dynamics Inverse System for Guide to a Moving Target |
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| GAO Jian,XU Hong,TONG Ming-an.Tracking Control of Missile''s Dynamics Inverse System for Guide to a Moving Target[J].Flight Dynamics,2008,26(5). |
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| Authors: | GAO Jian XU Hong TONG Ming-an |
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| Institution: | 1.College of Metrological Technology & Engineering;China Jiliang University;Hangzhou 310018;China;2.College of Electronic and Information Engineering;NWPU;Xi'an 710072;China |
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| Abstract: | Combined with the motion characteristics of target-missile,a tracking controller used in the Euler dynamics system of the centroid motion of a missile is designed based on the inverse system method and the theory of guidance.Some important factors for guidance process,i.e.,the flying state of target-missile,the control law and guidance law,decoupling and anti-interference characteristics,had been considered at the controller design process.The progressive tracking control is realized by controlling the exte... |
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| Keywords: | characteristics for target Euler equation inverse system method tracking control simulation |
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