Home           Contact us           FAQs           
    
     Journal Home     |     Aim & Scope    |    Author(s) Information      |     Editorial Board     |     MSP Download Statistics
    Abstract
2012 (Vol. 4, Issue: 20)
Article Information:

Discrete Neural Altitude Control for Hypersonic Vehicle Via Flight Path Angle Tracking

Shixing Wang, Bin Xu, Fuchun Sun and Yifu Jiang
Corresponding Author:  Shixing Wang 

Key words:  Discrete-time, hypersonic flight vehicle, neural network, , , ,
Vol. 4 , (20): 3930-3936
Submitted Accepted Published
December 20, 2011 April 23, 2012 October 15, 2012
Abstract:

In this study, the altitude control is analyzed for the longitudinal dynamics of a generic Hypersonic Flight Vehicle (HFV). By transforming altitude command into the tracking of flight path angle with fast dynamics, the system design is focusing on the control of the attitude subsystem. The virtual control is designed with nominal feedback and Neural Network (NN) approximation via back-stepping. Under the proposed controller, the Semiglobal Uniform Ultimate Boundedness (SGUUB) stability is guaranteed. The slow dynamics are transformed into the parameter estimation problem and the update law is designed. The simulation is presented to show the effectiveness of the proposed control approach.
Abstract PDF HTML
  Cite this Reference:
Shixing Wang, Bin Xu, Fuchun Sun and Yifu Jiang, 2012. Discrete Neural Altitude Control for Hypersonic Vehicle Via Flight Path Angle Tracking.  Research Journal of Applied Sciences, Engineering and Technology, 4(20): 3930-3936.
    Advertise with us
 
ISSN (Online):  2040-7467
ISSN (Print):   2040-7459
Submit Manuscript
   Current Information
   Sales & Services
Home  |  Contact us  |  About us  |  Privacy Policy
Copyright © 2015. MAXWELL Scientific Publication Corp., All rights reserved