中国运载火箭姿态控制技术发展与展望  

Review and Prospect of Attitude Control Technologies for China’s Launch Vehicle

作　　者：吴燕生 WU Yansheng(China Aerospace Science and Technology Corporation,Beijing 100048,China)

机构地区：[1]中国航天科技集团有限公司,北京100048

出　　处：《宇航学报》2023年第4期509-518,共10页Journal of Astronautics

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.

关 键 词：液体运载火箭 姿态控制 容错控制 可重构性 

分 类 号：V448[航空宇航科学与技术—飞行器设计]