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大气层内滚转角速度稳定动能拦截器姿态控制系统设计
引用本文:沈明辉,周伯昭,陈磊,吴瑞林.大气层内滚转角速度稳定动能拦截器姿态控制系统设计[J].国防科技大学学报,2006,28(4):133-136.
作者姓名:沈明辉  周伯昭  陈磊  吴瑞林
作者单位:国防科技大学,航天与材料工程学院,湖南,长沙,410073
摘    要:针对大气层内滚转角速度稳定动能拦截器具有反应快速、耦合性强等特点,本文首先分析了传统的小扰动法设计姿控系统的优缺点,然后提出了基于极点区域配置的变增益控制系统设计方法。该方法通过在整个参数空间寻求单一李亚普诺夫函数来保证系统的全局稳定,与小扰法相比,它不仅可保证理论上的稳定,而且离散计算量小。最后的仿真表明,基于该方法设计的控制器具有良好的控制性能。

关 键 词:动能拦截器  线性变参数  极点区域配置  线性矩阵不等式
文章编号:1001-2486(2006)04-0133-04
收稿时间:2006/3/20 0:00:00
修稿时间:2006年3月20日

Design of the Attitude Control System of the Atmospheric Kinetic Interceptor with Invariable Rolling Rate
SHEN Minghui,ZHOU Bozhao,CHEN Lei and WU Ruilin.Design of the Attitude Control System of the Atmospheric Kinetic Interceptor with Invariable Rolling Rate[J].Journal of National University of Defense Technology,2006,28(4):133-136.
Authors:SHEN Minghui  ZHOU Bozhao  CHEN Lei and WU Ruilin
Institution:College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:Considering that the atmospheric kinetic interceptor with invariable rolling rate has quick response and strong coupling,this paper firstly analyzes the advantage and disadvantage of the classic design method of the control system,and then it proposes the gain scheduling method based on the regional pole placement,which finds a Lyapunov function in the whole parameter space to guarantee system stability.Compared with the classic method,the new method is not only stable theoretically,but also convenient in calculation.Simulation results show that controller based on the method which be proposed in this paper has good performance.
Keywords:kinetic interceptor  Linear Parameter-Varying(LPV)  regional pole placement  Linear Matrix Inequality(LMI)
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