摘要
针对以冲压发动机为动力的远程战术导弹,描述了其飞行过程与特点。从制导律设计和控制律设计两个方面,综述了国内外相关技术的设计方法,论述了弹道优化技术、制导控制一体化、针对目标机动的制导律、BTT控制与速度控制技术的研究现状,探讨了冲压发动机导弹在制导控制方面的发展方向。
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.
出处
《航空兵器》
2016年第2期17-23,共7页
Aero Weaponry
