Paper Title:
Wind Shear Encountered Landing Control Based on CMACs
  Abstract

This paper presents an intelligent control scheme that uses different cerebellar model articulation controllers (CMACs) in aircraft automatic landing control. The proposed intelligent control system can act as an experienced pilot and guide the aircraft landed safely in wind shear condition. Lyapunov theory is applied to obtain adaptive learning rule and stability analysis is also provided. Furthermore, the proposed controllers are implemented in a DSP. The simulations by MatLab are demonstrated.

  Info
Periodical
Chapter
Chapter 8: Automation and Control
Edited by
Wen-Hsiang Hsieh
Pages
2351-2355
DOI
10.4028/www.scientific.net/AMM.284-287.2351
Citation
J. G. Juang, C. J. Cheng, T. C. Yang, "Wind Shear Encountered Landing Control Based on CMACs", Applied Mechanics and Materials, Vols. 284-287, pp. 2351-2355, Jan. 2013
Online since
January 2013
Price
US$ 28,-
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