Wind Shear Encountered Landing Control Based on CMACs

Abstract:

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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:

Edited by:

Wen-Hsiang Hsieh

Pages:

2351-2355

DOI:

10.4028/www.scientific.net/AMM.284-287.2351

Citation:

J. G. Juang et al., "Wind Shear Encountered Landing Control Based on CMACs", Applied Mechanics and Materials, Vols. 284-287, pp. 2351-2355, 2013

Online since:

January 2013

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Price:

$35.00

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