| 基于制导与控制一体化的导弹编队队形控制 |
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| 引用本文： | 刘新科,李大鹏,谭乐祖. 基于制导与控制一体化的导弹编队队形控制[J]. 火力与指挥控制, 2011, 8(8) |
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| 作者姓名： | 刘新科 李大鹏 谭乐祖 |
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| 作者单位： | 1. 西北工业大学,西安710072;海军大连舰艇学院,辽宁大连116001
2. 海军航空工程学院,山东烟台,264001 |
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| 摘 要： | 为了提高导弹编队协同作战队形控制能力,研究了基于制导与控制一体化思想的编队队形控制器设计问题。根据领弹-从弹的动力学以及运动学方程,推导出了领弹-从弹的相对运动模型,建立了领弹姿态信息与从弹舵偏角之间的关系,将从弹通道间的耦合项作为不确定项进行处理,并利用自适应神经网络理论设计了补偿器,对不确定项进行了处理。根据反演理论设计了编队队形控制器,能够对导弹编队队形进行有效的控制。
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| 关 键 词： | 制导与控制一体化 导弹编队 队形控制 反演 |
Research on Missile Formation Control Based on Integrated Guidance and Control |
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| LIU Xin-ke,LI Da-peng,TAN Le-zu. Research on Missile Formation Control Based on Integrated Guidance and Control[J]. Fire Control & Command Control, 2011, 8(8) |
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| Authors: | LIU Xin-ke LI Da-peng TAN Le-zu |
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| Affiliation: | LIU Xin-ke1,2,LI Da-peng3,TAN Le-zu3(1.Northwestern Polytechnical University,Xi'an 710072,China,2.Dalian Naval Academy,Dalian 116001,3.Naval Aeronautical Engineering Academy,Yantai 264001,China) |
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| Abstract: | Aimed at improving the missile formation control engagement,research the missile formation controller design based on integrated guidance and control theory.According to the dynamic equation and relative equation,deduce the relative motion model of the leader-follower missiles,and establish the relationship of the leader missile attitude and the follower missile rudder.See the coupling items of the follower missiles as the uncertainty,then design the adaptive neural network to approximate the uncertainties.... |
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| Keywords: | integrated guidance and control missile formation formation controller backstepping |
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