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| 一种变结构自适应中制导律设计 | |
| 引用本文： | 张勇,赵永涛,刘德伟.一种变结构自适应中制导律设计[J].海军航空工程学院学报,2008,23(1):18-20. |
| 作者姓名： | 张勇 赵永涛 刘德伟 |
| 作者单位： | 1. 海军航空工程学院,飞行器工程系,山东,烟台,264001 2. 海军航空工程学院,控制工程系,山东,烟台,264001 3. 72946部队,山东,淄博,255001 |
| 摘 要： | 应用广义预测拦截点的概念，基于变结构自适应理论，以相对速度偏角为滑模面，设计了一种新颖实用的变结构自适应中制导律并进行了仿真分析，结果显示导弹各项指标均很好地满足要求，验证了该中制导律的可行性与有效性。 |
| 关 键 词： | 广义预测拦截点 变结构自适应 相对速度偏角 中制导律 |
| 文章编号： | 1673-1522(2008)01-0018-03 |
| 修稿时间： | 2007年9月5日 |
Design of a Variable Structure Adaptive Midcourse Guidance Law |
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| ZHANG Yong,ZHAO Yong-tao and LIU De-wei.Design of a Variable Structure Adaptive Midcourse Guidance Law[J].Journal of Naval Aeronautical Engineering Institute,2008,23(1):18-20. | |
| Authors: | ZHANG Yong ZHAO Yong-tao and LIU De-wei |
| Institution: | ZHANG Yong, ZHAO Yong-tao, LIU De-wei ( 1. Naval Aeronautical and Astronautical University a. Department of Airborne Vehicle Engineering; b. Department of Control Engineering, Yantai Shangdong 264001, China; 2. The 72946^th Unit of PLA, Zibo Shandong 255001, China) |
| Abstract: | Applying the concept of the generalized interception spot, based on the variable structure adaptive theory and choosing the relative velocity deflection angle as the sliding-mode, a variable structure adaptive midcourse guidance law was designed. The simulation results showed that the indexes of the missile perfectly fulfilled the needs, which validated the feasibility and the effectively of the designed guidance law. |
| Keywords: | the generalized interception spot variable structure adaptive the relative velocity deflection angle midcourse guidance law |
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