基于特征点分段的导弹姿态全程滑态变结构控制研究  

Study on Global Variable Structure Control of Missile Attitude Based on Characteristic Points Subsection

作　　者：张云鹏[1] 缪栋[1] 刘云峰[1] 

机构地区：[1]西安第二炮兵工程学院,西安710025

出　　处：《战术导弹技术》2005年第2期48-51,共4页Tactical Missile Technology

摘　　要：将工程中常用的"分段定常"方法与全程滑态变结构控制理论相结合,提出了独特的时变全程滑态变结姆控制方法,并结合导弹姿态控制系统特点,提出了导弹姿态调节器设计方法和导弹姿态调节器控制算法,为实际应用提供了一定的理论基础与依据.The usual means of subsection constant in engineering and the global variable structure control theory are combined,and a unique time-variant global variable structure control method is put forward. Considering the character of missile attitude control system, a design method and a control algorithm of missile attitude adjuster are proposed,and theoretical basis for actual application is provided.

关 键 词：全程滑态变结构控制 姿态控制系统 分段定常 姿态调节器 时变性 

分 类 号：TJ765.23[兵器科学与技术—武器系统与运用工程]