海军航空工程学院学报2017，Vol.32Issue(3)：279-283,5.DOI:10.7682/j.issn.1673-1522.2017.03.005
基于扩张状态观测器的舰载机俯仰自适应滑模控制
ESO Based Adaptive Sliding Mode Control of Carrier-Based Aircraft Pitch Angle
摘要
Abstract
The need of priori information of the disturbance upper bound and chattering are the main shortcomings of tradi-tional adaptive sliding mode control. Based on the extended states observer, the robust of the adaptive sliding mode control was improved and the chattering was eliminated without any priori information of the disturbance upper bound. The im-proved adaptive sliding mode control was applied to the attitude control system of a carrier-based aircraft. The simulation results shows the effectiveness of the improvement.关键词
自适应滑模/扩张状态观测器/舰载机/姿态控制系统Key words
adaptive sliding mode/extended states observer/carrier-based aircraft/attitude control system引用本文复制引用
张勇,韩维,陈俊锋,崔世麒..基于扩张状态观测器的舰载机俯仰自适应滑模控制[J].海军航空工程学院学报,2017,32(3):279-283,5.基金项目
"泰山学者"建设工程专项经费资助 （）
