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基于制导与控制一体化的导弹编队队形控制

刘新科 李大鹏 谭乐祖

火力与指挥控制2011,Vol.8Issue(8):208-210,3.
火力与指挥控制2011,Vol.8Issue(8):208-210,3.

基于制导与控制一体化的导弹编队队形控制

Research on Missile Formation Control Based on Integrated Guidance and Control

刘新科 1李大鹏 2谭乐祖1

作者信息

  • 1. 西北工业大学,西安710072
  • 2. 海军大连舰艇学院,辽宁大连116001
  • 折叠

摘要

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. Design the formation controller based on backsteping theory, the controller can control the missile formation effectively.

关键词

制导与控制一体化/导弹编队/队形控制/反演

Key words

integrated guidance and control,missile formation,formation controller,backstepping

分类

信息技术与安全科学

引用本文复制引用

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):208-210,3.

火力与指挥控制

OA北大核心CSCDCSTPCD

1002-0640

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