Direct neural discrete control of hypersonic flight vehicle

This paper investigates the discrete neural control for flight path angle and velocity of a generic hypersonic flight vehicle (HFV). First, strict-feedback form is set up for the attitude subsystem considering flight path angle, pitch angle, and pitch rate by altitude-flight path angle transformatio...

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Bibliographic Details
Main Authors: Xu, Bin, Wang, Danwei, Sun, Fuchun, Shi, Zhongke
Other Authors: School of Electrical and Electronic Engineering
Format: Article
Language:English
Published: 2013
Subjects:
Online Access:https://hdl.handle.net/10356/98203
http://hdl.handle.net/10220/17651
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Institution: Nanyang Technological University
Language: English