多弹编队飞行控制技术研究  

Research on Flight Control Technology for Missiles Formation

作　　者：张奇[1] 

机构地区：[1]北京机电工程研究所,北京100074

出　　处：《导航定位与授时》2014年第2期31-34,共4页Navigation Positioning and Timing

摘　　要：针对未来复杂战场环境下反舰导弹编队协同攻击的技术需求,提出了一种多弹编队飞行控制的技术方案。采用基于分层递阶控制思想的多智能体系统结构,把多枚功能相同或者不同的导弹按照一定的原则组合成弹群,弹群中各导弹之间进行编队飞行、协同搜索、信息融合和协同攻击等方面的作战配合,实现对单个目标或多个目标的精确打击。该方案可以实现多发导弹的编队飞行控制,能够提高导弹编队的体系对抗能力。A missiles formation flight control scheme is put forward to regarding the requirement of anti - ship missile coop- erate attack in future complex war field. It used multi agent system structure based on the idea of delamination deliver, form a missile group by muhi missiles in same function or different function according to some rule, multi missiles in the foama- tion cooperated in formate flight, cooperate search, information amalgamate and cooperate attack, in order to accurate at- tack single target or multi target. The scheme can realize flight control for missiles formation, provide the formate ability of system countermine.

关 键 词：反舰导弹 编队飞行 制导控制 协同搜索 协同攻击 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]