摘要
从动力学建模、姿态控制器设计和设计仿真技术方面系统地梳理了中国液体运载火箭姿态控制技术的发展历程,总结了当前运载火箭姿态控制技术发展面临的问题和挑战。根据国外运载火箭姿态控制技术的发展趋势,结合后续中国运载火箭发展的技术需求,对姿态控制技术的未来发展进行展望,提出了下一阶段姿态控制技术发展的5项重点研究方向。
In this paper,the development history of the attitude control technologies for China’s liquid-propellant launch vehicles is systematically reviewed from three aspects of dynamic modeling,attitude controller designing and simulation technology.In addition,the current problems and challenges faced by the attitude control technology are summarized.According to the development trend of attitude control technology for the launch vehicles abroad and the technical requirements for the development of launch vehicles in China,the future development of the attitude control technology is prospected,and five key research directions for the next phase are put forward.
作者
吴燕生
WU Yansheng(China Aerospace Science and Technology Corporation,Beijing 100048,China)
出处
《宇航学报》
EI
CAS
CSCD
北大核心
2023年第4期509-518,共10页
Journal of Astronautics
关键词
液体运载火箭
姿态控制
容错控制
可重构性
Liquid launch vehicle
Attitude control
Fault-tolerant control
Reconfiguration
作者简介
吴燕生(1963-),男,博士,研究员,主要从事运载火箭总体设计、制导控制、故障诊断等方面的研究。通信地址:北京市海淀区阜成路16号(100048)。