Fault tolerant attitude controller for a class of additive faults via High-Order Sliding Modes

J. Dávila, J. Cieslak, D. Henry

Research output: Contribution to journalArticle

Abstract

© 2016 In this paper, an autopilot for attitude tracking is designed using disturbance compensation techniques. The proposed controller uses backstepping design procedure and combines the feedback linearization technique with high-order sliding-modes based identification for fault tolerant control. System faults and external disturbances are compensated by a differentiable term generated by means of the robust exact high-order sliding-modes differentiator. The control signal generated for the controller does not require filtration. Simulations illustrate the performance of the proposed controller in the rigid body model of an F-16 aircraft.
Original languageAmerican English
Pages (from-to)254-259
Number of pages228
JournalIFAC-PapersOnLine
DOIs
StatePublished - 1 Jan 2016
Externally publishedYes

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Controllers
Feedback linearization
Backstepping
Aircraft
Compensation and Redress

Cite this

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Fault tolerant attitude controller for a class of additive faults via High-Order Sliding Modes. / Dávila, J.; Cieslak, J.; Henry, D.

In: IFAC-PapersOnLine, 01.01.2016, p. 254-259.

Research output: Contribution to journalArticle

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