摘要
本文介绍了典型多模复合制导空地导弹的制导模式设计,对复合导引头的结构组成、工作原理、制导信息融合技术、制导信息过渡衔接切换技术、制导信息智能补偿技术作了阐述。最后,阐述了双模复合制导半实物仿真系统设计方案及典型双模复合制导半实物仿真系统组成原理及工作方式。
The typical guidance pattern design of multi-mode compound guidance missile is introduced,and the structure and the working principle of compound seeker,the guidance information fusion method,the guidance information transition connection and switching technology and the guidance information intelligent compensation technology are proposed.Finally,the design scheme and work mode of the dual-mode compound guidance hardware-in-the-loop simulation system are described.
作者
杨凯
卢莺
Yang Kai;Lu Ying(Xi’an Advanced Control Technologies Research Institute,Xi’an 710065,China)
出处
《航空兵器》
北大核心
2018年第1期20-26,共7页
Aero Weaponry
关键词
多模复合制导
信息融合
导引头
仿真系统
multi-mode compound guidance
information fusion
seeker
simulation system