Actuator failure detection and reconfigurable control for F-16 aircraft model

Fikret Caliskan; Chingiz Hajiyev

doi:10.1016/S1474-6670(17)35806-8

Actuator failure detection and reconfigurable control for F-16 aircraft model

Araştırma sonucu: Dergiye katkı › Konferans makalesi › bilirkişi

4 Atıf (Scopus)

Özet

In this paper, an approach to actuator failure detection and reconfigurable control for flight control system is presented. The effects of the actuator failures in die innovation process of the Kalman fdter are investigated, and a reconfiguration in control law is proposed. In the simulations, the longitudinal and lateral dynamics of an F-16 aircraft model is considered, and actuator failure detection and reconfigurable control are examined.

Orijinal dil	İngilizce
Sayfa (başlangıç-bitiş)	53-58
Sayfa sayısı	6
Dergi	IFAC-PapersOnLine
Hacim	36
Basın numarası	7
DOI'lar	https://doi.org/10.1016/S1474-6670(17)35806-8
Yayın durumu	Yayınlandı - 2003
Etkinlik	3rd IFAC Workshop on Automatic Systems for Building the Infrastructure in Developing Countries, DECOM-TT 2003 - Istanbul, Türkiye Süre: 26 Haz 2003 → 28 Haz 2003

Bibliyografik not

Publisher Copyright:
Copyright © 2003 IFAC.

Belgeye Erişim

10.1016/S1474-6670(17)35806-8

Diğer Dosyalar ve Linkler

Link to publication in Scopus

Alıntı Yap

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title = "Actuator failure detection and reconfigurable control for F-16 aircraft model",

abstract = "In this paper, an approach to actuator failure detection and reconfigurable control for flight control system is presented. The effects of the actuator failures in die innovation process of the Kalman fdter are investigated, and a reconfiguration in control law is proposed. In the simulations, the longitudinal and lateral dynamics of an F-16 aircraft model is considered, and actuator failure detection and reconfigurable control are examined.",

keywords = "Extended kalman filter, F-16 aircraft model, Failure detection, Reconfigurable control",

author = "Fikret Caliskan and Chingiz Hajiyev",

note = "Publisher Copyright: Copyright {\textcopyright} 2003 IFAC.; 3rd IFAC Workshop on Automatic Systems for Building the Infrastructure in Developing Countries, DECOM-TT 2003 ; Conference date: 26-06-2003 Through 28-06-2003",

year = "2003",

doi = "10.1016/S1474-6670(17)35806-8",

language = "English",

volume = "36",

pages = "53--58",

journal = "IFAC-PapersOnLine",

issn = "2405-8963",

publisher = "Elsevier B.V.",

number = "7",

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TY - JOUR

T1 - Actuator failure detection and reconfigurable control for F-16 aircraft model

AU - Caliskan, Fikret

AU - Hajiyev, Chingiz

PY - 2003

Y1 - 2003

N2 - In this paper, an approach to actuator failure detection and reconfigurable control for flight control system is presented. The effects of the actuator failures in die innovation process of the Kalman fdter are investigated, and a reconfiguration in control law is proposed. In the simulations, the longitudinal and lateral dynamics of an F-16 aircraft model is considered, and actuator failure detection and reconfigurable control are examined.

AB - In this paper, an approach to actuator failure detection and reconfigurable control for flight control system is presented. The effects of the actuator failures in die innovation process of the Kalman fdter are investigated, and a reconfiguration in control law is proposed. In the simulations, the longitudinal and lateral dynamics of an F-16 aircraft model is considered, and actuator failure detection and reconfigurable control are examined.

KW - Extended kalman filter

KW - F-16 aircraft model

KW - Failure detection

KW - Reconfigurable control

UR - https://www.scopus.com/pages/publications/19444386844

U2 - 10.1016/S1474-6670(17)35806-8

DO - 10.1016/S1474-6670(17)35806-8

M3 - Conference article

AN - SCOPUS:19444386844

SN - 2405-8963

VL - 36

SP - 53

EP - 58

JO - IFAC-PapersOnLine

JF - IFAC-PapersOnLine

IS - 7

T2 - 3rd IFAC Workshop on Automatic Systems for Building the Infrastructure in Developing Countries, DECOM-TT 2003

Y2 - 26 June 2003 through 28 June 2003

ER -

Actuator failure detection and reconfigurable control for F-16 aircraft model

Özet

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Belgeye Erişim

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