DocumentCode :
2101164
Title :
Implementations of real-time system identification using recursive techniques
Author :
Eure, Kenneth
Author_Institution :
NASA Langley Res. Center, Hampton, VA, USA
Volume :
6
fYear :
2002
fDate :
2002
Firstpage :
4807
Abstract :
Recursive identification techniques offer the ability to compute the transfer function of a system in realtime. This mathematical representation of a system may be used for various tasks such as health monitoring and feedback control. This paper presents the mathematical development of the Fast Transversal filter. It follows the work of Juang (1994), but adds to it by the introduction of a forgetting factor to accommodate changes in the plant. The FTF´s ability to track plant changes in real time offers applications in adaptive feedback control and adaptive fault detection. An example of the use of the FTF in feedback control is presented for a simple plant. Also, it is demonstrated that the FTF may be used to estimate a mathematical model of a Flight Control Computer for command signals during the Autoland phase. The example shown in this paper is for a B737 Autolander.
Keywords :
adaptive control; aircraft computers; aircraft landing guidance; fault diagnosis; feedback; filtering theory; identification; real-time systems; recursive estimation; Autoland phase; B737 Autolander; adaptive fault detection; adaptive feedback control; command signals; fast transversal filter; feedback control; flight control computer; forgetting factor; health monitoring; mathematical model; real-time system identification; recursive techniques; simple plant; transfer function; Adaptive control; Application software; Fault detection; Feedback control; Monitoring; Programmable control; Real time systems; System identification; Transfer functions; Transversal filters;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2002. Proceedings of the 2002
ISSN :
0743-1619
Print_ISBN :
0-7803-7298-0
Type :
conf
DOI :
10.1109/ACC.2002.1025419
Filename :
1025419
Link To Document :
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