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

^*Bu çalışma için yazışmadan sorumlu yazar

Araştırma çıktısı: Dergi yayını › Konferans makalesi › Hakem

12 Atıf (Scopus)

Özet

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.

Orijinal dil	İngilizce
Sayfa (başlangıç-bitiş)	1220-1224
Sayfa sayısı	5
Dergi	Proceedings of the American Control Conference
Hacim	2
DOI'lar	https://doi.org/10.1109/acc.2000.876694
Yayın durumu	Yayınlandı - 2000
Etkinlik	2000 American Control Conference - Chicago, IL, USA Süre: 28 Haz 2000 → 30 Haz 2000

Belgeye Erişim

10.1109/acc.2000.876694

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Link to publication in Scopus

Alıntı Yap

@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

Özet

Belgeye Erişim

Diğer Dosyalar ve Linkler

Parmak izi

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