运载火箭姿态控制技术的发展趋势和展望  

Development Trend and Prospect of Attitude Control Technologies of Launch Vehicle

作　　者：张卫东[1] 刘玉玺 刘汉兵 丁秀峰 张开宝 Zhang Weidong Liu Yuxi Liu Hanbing Ding Xiufeng Zhang Kaibao(Shanghai Academy of Spaceflight Technology, Shanghai 201109, China Shanghai Aerospace System Engineering Institute, Shanghai 201109, China)

机构地区：[1]上海航天技术研究院,上海201109 [2]上海宇航系统工程研究所,上海201109

出　　处：《航天控制》2017年第3期85-89,共5页Aerospace Control

摘　　要：对国外运载火箭的姿态控制技术发展进行了梳理。根据国外运载火箭姿控技术的发展趋势,并结合国内运载火箭的发展方向,提出了几种可能应用于国内运载火箭的姿态控制方法,并给出了这几种姿态控制技术的工程实现方法和途径。分析表明,这几种控制方法对克服火箭参数不确定性、提高火箭姿控系统的鲁棒性具有明显优势。The development of attitude control technologies of overseas launch vehicle are reviewed in the paper. According to the development trend of overseas launch vehicle and the development direction of domes- tic launch vehicle, several attitude control methods are proposed, which will be applied to the domestic launch vehicle in the future. The approaches and ways of engineering realization are introduced. The theory analysis shows the methods have virtues for overcoming the uncertain parameters and improving the robust-

关 键 词：运载火箭 姿态控制 发展趋势 工程实现 

分 类 号：V448.1[航空宇航科学与技术—飞行器设计]