Discrete flight path angle tracking control of hypersonic flight vehicles via multi-rate sampling

This paper presents the flight path angle tracking control of the longitudinal dynamics of a generic hypersonic flight vehicle(HFV). Due to the use of digital computers and microprocessors for controls applications, the discrete hypersonic flight control is investigated. The altitude command is tran...

全面介紹

Saved in:
書目詳細資料
Main Authors: Xu, Bin, Wang, Danwei, Yang, Chenguang, Li, Jing, Wang, Shixing
其他作者: School of Electrical and Electronic Engineering
格式: Conference or Workshop Item
語言:English
出版: 2013
在線閱讀:https://hdl.handle.net/10356/98868
http://hdl.handle.net/10220/12652
標簽: 添加標簽
沒有標簽, 成為第一個標記此記錄!