空地导弹复合制导模式设计及仿真技术研究  

Multi-Mode Compound Guidance Missile's Pattern Design and Simulation Technology Research

作　　者：杨凯 卢莺 Yang Kai;Lu Ying(Xi’an Advanced Control Technologies Research Institute,Xi’an 710065,China)

机构地区：[1]西安现代控制技术研究所,西安710065

出　　处：《航空兵器》2018年第1期20-26,共7页Aero Weaponry

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.

关 键 词：多模复合制导 信息融合 导引头 仿真系统 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程]