一体化制导综合控制平台的研究
Research on Integrated Guidance and Control Platform
黑蕾 1陈肖雨 1王江1
作者信息
- 1. 中国航天科技集团公司第四研究院第四十一研究所 115 室,西安 710025
- 折叠
摘要
针对弹上核心部件高集成度、高性能、低成本的需求,采用综合处理集成设计理念,设计一款新型弹上飞控制导组合平台.集成多个弹上部件功能,简化系统构架,通过多次飞行试验.试验结果表明,该平台性能稳定、结构紧凑、可靠性强、控制精度高,满足导弹控制系统设计要求.
Abstract
In order to meet the requirements of high integration,high performance and low cost of the core components on the missile,a new type of flight control and guidance integrated platform on the missile is designed by using the integrated design concept of comprehensive processing,which integrates the functions of multiple components on the missile,simplifies the system architecture,and has passed many flight tests.The test results show that the platform has stable performance,compact structure,high reliability and high control precision,and meets the design requirements of missile control system.
关键词
一体化/制导组合/弹上部件Key words
integration/guidance combination/missile-borne components引用本文复制引用
出版年
2025
国家科技期刊平台
NSTL
万方数据