首页 | 本学科首页   官方微博 | 高级检索  
     检索      

一种利用动量轮的弹头姿态控制系统概念研究
引用本文:雍恩米,唐国金.一种利用动量轮的弹头姿态控制系统概念研究[J].宇航学报,2006,27(3):396-401,415.
作者姓名:雍恩米  唐国金
作者单位:国防科技大学航天与材料工程学院,长沙,410073
摘    要:对一种以动量轮为执行机构的具有中性静稳定外形的再入弹头姿态控制系统进行了概念研究。从动量矩定理和中性静稳定原理阐述了这种控制方案从理论上是可行的。推导了动量轮控制弹头的姿态动力学方程,并基于分离时间尺度方法设计了姿态控制系统。对该姿态控制系统仿真研究表明:1)姿态角跟踪回路性能良好;2)在不需要太大的动量轮控制输入力矩的情况下,能实现滚动通道稳定控制;3)俯仰和偏航通道的正弦跟踪需要相对较大动量矩的动量轮作为执行机构来实现高精度跟踪控制。

关 键 词:动量轮  分离时间尺度法  弹头姿态控制  概念研究
文章编号:1000-1328(2006)03-0396-06
收稿时间:2005-04-27
修稿时间:2005-04-272005-12-15

The Conceptional Study of Using Moment Wheels for the Attitude Control of a Warhead
YONG En-mi,TANG Guo-jin.The Conceptional Study of Using Moment Wheels for the Attitude Control of a Warhead[J].Journal of Astronautics,2006,27(3):396-401,415.
Authors:YONG En-mi  TANG Guo-jin
Institution:College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:The conceptional study of a moment wheels control system for a reentry warhead of indifferently static stability is presented.The feasibility of this proposal is theoretically demonstrated by momentum theorem and indifferently static stability conception.Then we derived the attitude dynamic equations of the moment wheels controlled warhead,and formalized the attitude control strategy by two time scales approach.Simulation studies indicate the following features:1)the attitude angle velocity control loop has a good tracking performance;2)Small control input values of moment wheels can stabilize the roll channel;3)The sinusoidal trajectory tracking of pitch and yaw channels requires relatively large angular moment wheels to achieve high precision.
Keywords:Momentum wheels  Two time scales approach  Attitude control of warhead  Conceptional study
本文献已被 CNKI 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号