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...

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Bibliographic Details
Main Authors: Xu, Bin, Wang, Danwei, Yang, Chenguang, Li, Jing, Wang, Shixing
Other Authors: School of Electrical and Electronic Engineering
Format: Conference or Workshop Item
Language:English
Published: 2013
Online Access:https://hdl.handle.net/10356/98868
http://hdl.handle.net/10220/12652
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Institution: Nanyang Technological University
Language: English