CASIA OpenIR  > 综合信息系统研究中心
Time-varying Spectrum Based Active Disturbance Rejection Control for Hypersonic Reentry Vehicle
Zhiqiang Pu1; Jianhong Zhang2; Ruyi Yuan; Jianqiang Yi
2016
会议名称2016 IEEE International Conference on Mechatronics and Automation
会议录名称Proceedings of 2016 IEEE International Conference on Mechatronics and Automation
页码1507-1512
会议日期August 7-10, 2016
会议地点Harbin, China
摘要This paper proposes a robust attitude control strategy for hypersonic reentry vehicles which combines novel time-varying spectrum based active disturbance rejection control techniques with a basic stabilizing controller. These techniques include time-varying tracking differentiator (TTD) and timevarying extended state observer (TESO). By adopting timevarying bandwidth, TTD can adaptively arrange transient processes for either abrupt or smooth reference commands. Also by designing time-varying bandwidth logic, TESO can not only estimate total disturbance well, but also suppress peaking phenomenon resulting from initial reentry condition dispersion. Several simulations are conducted which demonstrate that the
proposed control strategy exhibits both good attitude tracking ability and great design flexibility.
关键词Hypersonic Vehicle Reentry Active Disturbance Rejection Control Time-varying Spectrum
收录类别EI
文献类型会议论文
条目标识符http://ir.ia.ac.cn/handle/173211/12365
专题综合信息系统研究中心
通讯作者Zhiqiang Pu
作者单位1.Institute of Automation, Chinese Academy of Sciences
2.Beijing Aerospace Automatic Control Institute
推荐引用方式
GB/T 7714
Zhiqiang Pu,Jianhong Zhang,Ruyi Yuan,et al. Time-varying Spectrum Based Active Disturbance Rejection Control for Hypersonic Reentry Vehicle[C],2016:1507-1512.
条目包含的文件 下载所有文件
文件名称/大小 文献类型 版本类型 开放类型 使用许可
07558787.pdf(308KB)会议论文 开放获取CC BY-NC-SA浏览 下载
个性服务
推荐该条目
保存到收藏夹
查看访问统计
导出为Endnote文件
谷歌学术
谷歌学术中相似的文章
[Zhiqiang Pu]的文章
[Jianhong Zhang]的文章
[Ruyi Yuan]的文章
百度学术
百度学术中相似的文章
[Zhiqiang Pu]的文章
[Jianhong Zhang]的文章
[Ruyi Yuan]的文章
必应学术
必应学术中相似的文章
[Zhiqiang Pu]的文章
[Jianhong Zhang]的文章
[Ruyi Yuan]的文章
相关权益政策
暂无数据
收藏/分享
文件名: 07558787.pdf
格式: Adobe PDF
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。