EKF based surface fault detection and reconfiguration in aircraft control systems

F. Caliskan; Ch M. Hajiyev

doi:10.1109/acc.2000.876694

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 journal › Conference article › peer-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 language	English
Pages (from-to)	1220-1224
Number of pages	5
Journal	Proceedings of the American Control Conference
Volume	2
DOIs	https://doi.org/10.1109/acc.2000.876694
Publication status	Published - 2000
Event	2000 American Control Conference - Chicago, IL, USA Duration: 28 Jun 2000 → 30 Jun 2000

Access to Document

10.1109/acc.2000.876694

Cite this

@article{180dc744a3294e53ab404463743e104c,

title = "EKF based surface fault detection and reconfiguration in aircraft control systems",

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.",

author = "F. Caliskan and Hajiyev, \{Ch M.\}",

year = "2000",

doi = "10.1109/acc.2000.876694",

language = "English",

volume = "2",

pages = "1220--1224",

journal = "Proceedings of the American Control Conference",

issn = "0743-1619",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "2000 American Control Conference ; Conference date: 28-06-2000 Through 30-06-2000",

}

TY - JOUR

T1 - EKF based surface fault detection and reconfiguration in aircraft control systems

AU - Caliskan, F.

AU - Hajiyev, Ch M.

PY - 2000

Y1 - 2000

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/0034539893

U2 - 10.1109/acc.2000.876694

DO - 10.1109/acc.2000.876694

M3 - Conference article

AN - SCOPUS:0034539893

SN - 0743-1619

VL - 2

SP - 1220

EP - 1224

JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

T2 - 2000 American Control Conference

Y2 - 28 June 2000 through 30 June 2000

ER -

EKF based surface fault detection and reconfiguration in aircraft control systems

Abstract

Access to Document

Other files and links

Fingerprint

Cite this