EKF based surface fault detection and reconfiguration in aircraft control systems

F. Caliskan*, Ch M. Hajiyev

*Corresponding author for this work

Research output: Contribution to journalConference articlepeer-review

12 Citations (Scopus)

Abstract

In this paper, a surface fault detection algorithm based on the Extended Kalman Filter (EKF) is presented. The innovation- the difference between the actual plant states and the plant states identified by the EKF are evaluated for the fault detection and identification, and the control reconfiguration procedure is executed by considering the identified control distribution matrix.

Original languageEnglish
Pages (from-to)1220-1224
Number of pages5
JournalProceedings of the American Control Conference
Volume2
DOIs
Publication statusPublished - 2000
Event2000 American Control Conference - Chicago, IL, USA
Duration: 28 Jun 200030 Jun 2000

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