| 智能滑模变结构制导律 |
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| 引用本文： | 王志清,李小兵,卓启明.智能滑模变结构制导律[J].上海航天,2011,28(1):32-36. |
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| 作者姓名： | 王志清 李小兵 卓启明 |
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| 作者单位： | 1. 空军工程大学导弹学院,陕西,三原,713800
2. 中国人民解放军驻上海航天制造厂军事代表室,上海,200245 |
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| 摘 要： | 基于零化反导导弹的脱靶量,用变结构控制理论和非线性运动学方程推导了一种能适应目标作大机动的滑模变结构制导律。设计了一种新颖的模糊逻辑控制器,通过嵌入专家经验,实现了导引律系数的智能改变,建立了目标作螺旋机动的数学模型。末制导仿真结果表明：智能滑模变结构制导律在拦截三维螺旋机动目标时具有响应快速性,视线角速率和脱靶量较小,对高速大机动目标有较好的拦截效果。
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| 关 键 词： | 反导导弹 脱靶量 螺旋机动 变结构 智能 |
Research on Intelligent Sliding-Mode Variable Structure Guidance Law |
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| WANG Zhi-qing,LI Xiao-bing,ZHUO Qi-ming.Research on Intelligent Sliding-Mode Variable Structure Guidance Law[J].Aerospace Shanghai,2011,28(1):32-36. |
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| Authors: | WANG Zhi-qing LI Xiao-bing ZHUO Qi-ming |
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| Institution: | WANG Zhi-qing1,LI Xiao-bing1,ZHUO Qi-ming2(1.The Missile Institute of Air Force Engineering University,Sanyuan Shaanxi 713800,China,2.The CPLA Represent Office in Shanghai Aerospace Equipments Manufacturer,Shanghai 200245,China) |
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| Abstract: | A variable structure guidance law using variable structure control theoretic and non-linear equation which could be used for intercepting severity mobility target was put forward based on near zero-miss distance of the antimissile missile in this paper.A novel fuzzy logic controller was designed.By embedded experience of experts into rules,the controller could adjust the coefficients in the guidance law.The mathematic model of target with gyroidal maneuver was given out.The simulation results of the termina... |
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| Keywords: | Anti tactical ballistic missile Miss distance Gyroidal maneuver Variable structure Intelligent |
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