Please use this identifier to cite or link to this item: http://scholarbank.nus.edu.sg/handle/10635/115476
Title: Reliable automatic landing control against actuator stuck faults
Authors: Liao, F. 
Wang, J.L.
Poh, E.K.
Li, D.
Keywords: Actuator stuck faults
Affine parameter-dependent lyapunov functions
Automatic landing
H 2 norm
Reliable control
Issue Date: 2004
Source: Liao, F.,Wang, J.L.,Poh, E.K.,Li, D. (2004). Reliable automatic landing control against actuator stuck faults. Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 4 : 2283-2295. ScholarBank@NUS Repository.
Abstract: This paper presents a new LMI-based approach for developing reliable automatic landing controllers which can tolerate actuator stuck faults. The H 2 control technique is used to guarantee tracking performance with respect to a given glide slope trajectory. A realistic fighter aircraft model is studied to illustrate the proposed approach. Nonlinear simulation under various faults and wind disturbances are included in this study. Simulation results show that the proposed reliable controller design approach can achieve zero steady-state tracking error, robustness against wind disturbances and reliability against actuator stuck faults. Copyright © 2004 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
Source Title: Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference
URI: http://scholarbank.nus.edu.sg/handle/10635/115476
ISBN: 1563476703
Appears in Collections:Staff Publications

Show full item record
Files in This Item:
There are no files associated with this item.

Page view(s)

30
checked on Jan 14, 2018

Google ScholarTM

Check


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.