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  1. National Taiwan Ocean University Research Hub
  2. 電機資訊學院
  3. 通訊與導航工程學系
Please use this identifier to cite or link to this item: http://scholars.ntou.edu.tw/handle/123456789/18134
Title: Intelligent Landing Control Using Linearized Inverse Aircraft Model
Authors: Jih-Gau Juang 
Hao-Hsiang Chang
Kai-Chung Cheng
Keywords: Intelligent control;Aircraft;aerospace control;Inverse problems;Automatic control;Neural networks;Safety;Intelligent systems;intelligent networks;Robustness
Issue Date: 2002
Publisher: IEEE
Journal Volume: 4
Start page/Pages: 3269-3274
Conference: Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301)
Anchorage, AK, USA
Abstract: 
Neural network applications to aircraft automatic landing control based on linearized inverse aircraft model are presented. Conventional automatic landing systems 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 study is to investigate the use of neural networks with linearized inverse aircraft model in automatic landing systems and to make these systems more intelligent. Current flight control law is adopted in the intelligent controller design. Tracking performance and robustness are demonstrated through software simulations. This paper presents five different neural network controllers to improve the performance of conventional automatic landing systems based on the linearized inverse aircraft model. Simulation results show that the neural network controller can successfully expand the safety envelope to include more hostile environments such as severe turbulence
URI: http://scholars.ntou.edu.tw/handle/123456789/18134
ISBN: 0-7803-7298-0
ISSN: 0743-1619
DOI: 10.1109/ACC.2002.1025295
Appears in Collections:通訊與導航工程學系

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