航空兵器Issue(2)：17-23,7.DOI:10.19297/j.cnki.41-1228/tj.2016.02.003
基于冲压发动机技术的远程战术导弹制导与控制发展综述
Review on Development of Guidance and Control for Long-Range Tactical Missile Based on Ramjet Technique
马立群 1段朝阳1
作者信息
- 1. 中国空空导弹研究院，河南洛阳 471009
- 折叠
摘要
Abstract
The flight process and characteristics of long-range tactical missile powered by ramjet are described.The design methods for guidance law and control law both at home and abroad are overviewed. Then the research status of key techniques are analyzed, including the trajectory optimization, integrated guidance and control, guidance law design for target maneuver, bank-to-turm( BTT) control and velocity control technology.At last, the trend of the ramjet missile in the guidance and control is discussed.关键词
冲压发动机/远程导弹/制导与控制/BTT导弹/一体化设计Key words
ramjet/long-range missile/guidance and control/BTT missile/integrate design分类
军事科技引用本文复制引用
马立群,段朝阳..基于冲压发动机技术的远程战术导弹制导与控制发展综述[J].航空兵器,2016,(2):17-23,7.
