摘要
阐述了现代战机导引系统的功能、结构与工作方式。基于对导弹制导等相关问题的深入研究,以及对战机导引的特点分析,阐述了战机导引控制律设计中应当解决的关键技术与研究途径,包括远距导引、近距导引和机动导引不同阶段的特点、捕获域的定义与计算方法、战机导引律研究特点及其基本工作模态。本研究可为新一代战机导引系统的研制提供参考。
The general description of pursuit-attacking guidance of a modern fighter is addressed first.Referring to the study on other related-research fields, such as missile guidance, and characteristics of pursuit-attack guidance of a fighter. Some key aspects, according to three basic guidance phases, i.e., pursuit guidance, attacking guidance and agile-flight guidance, and the related research idea are discussed then. Finally, three important problems, i.e., computation of capture set, the design of the guidance laws and basic operation modes of guidance system, are proposed and studied. This paper may be helpful to the design of pursuit-attacking guidance systems of the modern fighter.
出处
《飞行力学》
CSCD
2004年第4期1-4,共4页
Flight Dynamics
基金
空装预研基金资助项目(402050102)
关键词
战机
目标
导引
攻击
捕获域
工作模态
fighter
target
guidance
attack
capture set
operation mode
