Decisional Autonomy of Approach and Landing Phase for Civil Aviation Aircraft using Dual Fuzzy Neural Network

Author:

Xu Kai Jun1

Affiliation:

1. Civil Aviation Flight University of China (CAFUC)

Abstract

This paper presents the dual fuzzy neural network, designed the decisional autonomy flight controller for civil aviation aircraft in approach and landing phase. Real-time learning method was applied to train the neural network using the gradient-descent of an error function to adaptively update weights. Adaptive learning rates were obtained through the analysis of Lyapunov stability to guarantee the convergence of learning. Conventional automatic landing system (ALS) can provide a smooth landing, which is essential to the comfort of passengers. However, these systems work only within a specified operational safety envelope. When the conditions are beyond the envelope, such as turbulence or wind shear, they often cannot be used. The objective of this paper is to investigate the use of dual fuzzy neural network in ALS and to make that system more intelligent.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Reference11 articles.

1. Federal Aviation Administration, Automatic Landing Systems, Jan. 1971. AC 20-57A.

2. C. E. Cohen et al., Automatic landing of a 737 using GNSS integrity beacons, in Proc. ISPA, 995, p.247–252.

3. Advanced Auto Landing System from Swiss Federal Aircraft Factory, Real-Time Journal, 1995. Sprint.

4. C. C. Jorgensen and C. Schley, A neural network baseline problem for control of aircraft flare and touchdown, in Neural Networks for Control. Cambridge, MA: MIT Press, 1991, p.403–425.

5. M. Idan, M.D. Johnson, M.J. Calise, A hierarchical approach to adaptive control for improved flight safety, AIAA Journal of Guidance, Control, and Dynamics 25 (6) (2002) 1012.

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