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

Abstract : 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.
Type de document :
Communication dans un congrès
IFAC. 4th IFAC International Conference on Intelligent Control and Automation Sciences, Jun 2016, Reims, France. 〈http://icons2016.univ-reims.fr/〉
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https://hal.archives-ouvertes.fr/hal-01306943
Contributeur : Jérome Cieslak <>
Soumis le : lundi 25 avril 2016 - 20:44:51
Dernière modification le : jeudi 11 janvier 2018 - 06:21:09

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  • HAL Id : hal-01306943, version 1

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Jorge Davila, Jérome Cieslak, David Henry. Fault tolerant attitude controller for a class of additive faults via High-Order Sliding Modes. IFAC. 4th IFAC International Conference on Intelligent Control and Automation Sciences, Jun 2016, Reims, France. 〈http://icons2016.univ-reims.fr/〉. 〈hal-01306943〉

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