偏移量(计算机科学)
导弹
运动学
控制理论(社会学)
约束(计算机辅助设计)
制导系统
导弹制导
比例导航
计算机科学
法学
工程类
航空航天工程
物理
人工智能
经典力学
机械工程
政治学
控制(管理)
程序设计语言
作者
Shuai Zhenan,Rui Lv,Wei Chen,Ruisheng Sun,Yuan Li
出处
期刊:Lecture notes in electrical engineering
日期:2023-01-01
卷期号:: 7088-7096
标识
DOI:10.1007/978-981-19-6613-2_683
摘要
To solve the problem of multiply missiles with varying velocities attacking the target simultaneously, a cooperative guidance strategy with impact time and angle constraint is proposed. Firstly, a three-dimensional cooperative guidance model is presented by establishing the kinematics and dynamics equations of each missile, the relative motion relationship between the missile and the target is derived. Then a time-to-go method with time-varying velocities is designed. Considering the constraint of field of view angle and attack angle, the three-dimensional cooperative guidance law is designed based on offset proportional guidance method. Finally, simulation results verify the effectiveness and superiority of the proposed guidance law.
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