Title :
Intelligent landing control using linearized inverse aircraft model
Author :
Juang, Jih-Gau ; Chang, Hao-Hsiang ; Cheng, Kai-Chung
Author_Institution :
Dept. of Guidance & Commun. Technol., Nat. Taiwan Ocean Univ., Keelung, Taiwan
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.
Keywords :
aerospace control; aerospace simulation; aircraft landing guidance; intelligent control; aircraft automatic landing control; flight control law; intelligent controller design; intelligent landing control; linearised inverse aircraft model; neural network; operational safety envelope; robustness; safety envelope; smooth landing; software simulations; Aerospace control; Aircraft; Automatic control; Intelligent control; Intelligent networks; Intelligent systems; Inverse problems; Neural networks; Robustness; Safety;
Conference_Titel :
American Control Conference, 2002. Proceedings of the 2002
Print_ISBN :
0-7803-7298-0
DOI :
10.1109/ACC.2002.1025295