Research on the missile formation keeping optimal control for cooperative engagement

被引：0
|
作者：
Wei C.-Z. [1 ]
Guo J.-F. [1 ]
Cui N.-G. [1 ]
机构：
[1] Dept. of Astronautic Engineering, Harbin Institute of Technology
来源：
Yuhang Xuebao/Journal of Astronautics | 2010年 / 31卷 / 04期
关键词：
Cooperative engagement; Formation flight; Formation keeping; Missile; Optimal control;
D O I：
10.3873/j.issn.1000-1328.2010.04.017
中图分类号：
学科分类号：
摘要：
Aimed at the needs of missile cooperative engagement mission, designed the optimal control to keep missile formation. Analyse the frame of missile formation control system from the view of cooperative engagement system. Based on the missile kinematics in relative coordinate frame, structured the missile relative motion model straight, which made the process of motion between missiles became transparent. Considered the states of leader as perturbation variable, designed the missile formation keeping optimal control based on linear quadric optimal theory. Simulations demonstrate that the formation keeping optimal control is capable of restraining perturbation variable brought by model, leader states and linearizing analyse, and is able to implement the reconfiguring and keeping expected formation rapidly, stably and exactly.
引用
收藏
页码：1043 / 1050
页数：7
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