海军航空工程学院学报Issue(3)：225-229,5.DOI:10.7682/j.issn.1673-1522.2014.03.006
基于PIDNN变结构理论的新型弹道导弹姿控系统设计
Design of Attitude Control System for New Ballistic Missiles Based on PIDNN Variable Structure Control Theory
袁钢 1施建洪 2李瑞涛2
作者信息
- 1. 海军装备部，上海200436
- 2. 海军航空工程学院控制工程系，山东烟台264001
- 折叠
摘要
Abstract
The design problem of attitude control system for new ballistic missiles was studied to deal with the uncertainty of parameters and disturbance. Firstly, the model of the object was described to separate certain and uncertain parameters. Secondly, variable structure controller was designed on the assumption that upper bound of uncertainties was known. Thirdly, on the assumption that upper bound of uncertainties was unknown, PIDNN variable structure controller was de-signed by integrating variable structure control theory with PIDNN theory which was used to estimate the upper bound of uncertainties and the stability of the system was proved by Lyapunov theory. Finally, the simulation was presented to dem-onstrate the effectiveness of the proposed method.关键词
新型弹道导弹/不确定上界/变结构控制/比例-积分-微分神经网络Key words
new ballistic missiles/upper bound of uncertainty/variable structure control/PIDNN分类
军事科技引用本文复制引用
袁钢,施建洪,李瑞涛..基于PIDNN变结构理论的新型弹道导弹姿控系统设计[J].海军航空工程学院学报,2014,(3):225-229,5.
