上海航天（中英文）2025，Vol.42Issue(z1)：166-173,8.DOI:10.19328/j.cnki.2096-8655.2025.S1.020
长征二号丁运载火箭控制系统技术发展路线综述
Development of Control System Technology on Long March 2D Launch Vehicle
张鲲鹏 1朱蕾蕾 1石志华 1张桃源 1杨涛 1黄飞1
作者信息
- 1. 上海航天控制技术研究所,上海 201109
- 折叠
摘要
Abstract
Long March 2D(LM-2D)launch vehicle is one important member of China's Long March family.The control system,as a core subsystem of LM-2D,encompasses functions such as navigation,guidance and attitude control.The evolution of the control system is categorized into three developmental phases based on the goals of ensuring mission success,achieving high reliability and maximizing cost-effectiveness.Key technologies were developed including integrated navigation,iterative guidance,quaternion attitude control,redundancy fault diagnosis solutions.These innovations have facilitated advances in inertial,servo,and electronic products,enhanced system reliability and shortened development cycles.This paper comprehensively elaborates on the control system architectures and representative technologies across all three phases,and proposes potential directions for future development.关键词
运载火箭/控制系统/发展综述/冗余改进/惯性产品Key words
launch vehicle/control system/technology development review/redundancy scheme/inertial product分类
航空航天引用本文复制引用
张鲲鹏,朱蕾蕾,石志华,张桃源,杨涛,黄飞..长征二号丁运载火箭控制系统技术发展路线综述[J].上海航天（中英文）,2025,42(z1):166-173,8.
