• Türkçe
    • English
  • English 
    • Türkçe
    • English
  • Login
View Item 
  •   DSpace@Artvin
  • Fakülteler
  • Mühendislik Fakültesi
  • Elektrik - Elektronik Mühendisliği Bölümü
  • Elektrik - Elektronik Mühendisliği Bölümü Koleksiyonu - Makaleler
  • View Item
  •   DSpace@Artvin
  • Fakülteler
  • Mühendislik Fakültesi
  • Elektrik - Elektronik Mühendisliği Bölümü
  • Elektrik - Elektronik Mühendisliği Bölümü Koleksiyonu - Makaleler
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

A passive fault-tolerant switched control approach for linear multivariable systems: application to a quadcopter unmanned aerial vehicle model

Access

info:eu-repo/semantics/closedAccess

Date

2020

Author

Başak, Hasan
Kemer, Emre
Prempain, Emmanuel

Metadata

Show full item record

Citation

Başak, H., Kemer, E., & Prempain, E. (2020). A Passive Fault-Tolerant Switched Control Approach for Linear Multivariable Systems: Application to a Quadcopter Unmanned Aerial Vehicle Model. Journal of Dynamic Systems, Measurement, and Control, 142(3).

Abstract

This paper proposes synthesis algorithms for the design of passive state- and output-feedback fault-tolerant controllers. Sufficient conditions for the existence and the construction of such fault-tolerant controllers are given in terms of linear matrix inequalities (LMIs) which can be solved efficiently. The state-feedback fault-tolerant controller consists of a family of state-feedback gains switched appropriately according to a stabilizing switching signal so that the closed-loop system satisfies a performance requirement expressed in terms of system L-2 norm. Similarly, the output feedback controller consists of a family of full-order linear, time-invariant controllers switched according to a stabilizing signal that depends only on the controller states. Both approaches are passive in the sense that they do not rely on the detection and/or the estimation of the faults. The proposed approaches are tested on a nonlinear model of a quadcopter. Simulation results show that satisfactory stability, tracking, and disturbance rejection are maintained despite of time-varying actuator faults.

Source

Journal Of Dynamic Systems Measurement And Control-Transactions Of The Asme

Volume

142

Issue

3

URI

https://hdl.handle.net/11494/2012

Collections

  • Elektrik - Elektronik Mühendisliği Bölümü Koleksiyonu - Makaleler [36]
  • WoS İndeksli Yayınlar Koleksiyonu [685]



DSpace software copyright © 2002-2015  DuraSpace
Contact Us | Send Feedback
Theme by 
@mire NV
 

 




| Policy | Guide | Contact |
Advanced Search

sherpa/romeo

Browse

All of DSpaceCommunities & CollectionsBy Issue DateAuthorsInstitution AuthorORCIDTitlesSubjectsTypeLanguageDepartmentCategoryPublisherAccess TypeThis CollectionBy Issue DateAuthorsInstitution AuthorORCIDTitlesSubjectsTypeLanguageDepartmentCategoryPublisherAccess Type

My Account

LoginRegister

Statistics

View Google Analytics Statistics

DSpace software copyright © 2002-2015  DuraSpace
Contact Us | Send Feedback
Theme by 
@mire NV
 

 


|| Policy || Guide || Library || Artvin Çoruh University || OAI-PMH ||

Artvin Çoruh University, Artvin, Turkey
If you find any errors in content, please contact:

Creative Commons License
Artvin Çoruh University Institutional Repository is licensed under a Creative Commons Attribution-NonCommercial-NoDerivs 4.0 Unported License..

DSpace@Artvin:


DSpace 6.2

tarafından İdeal DSpace hizmetleri çerçevesinde özelleştirilerek kurulmuştur.