Super twisting control algorithm for the attitude tracking of a four rotors UAV

This paper deals with the design and implementation of a nonlinear control algorithm for the attitude tracking of a four-rotor helicopter known as quadrotor. This algorithm is based on the second order sliding mode technique known as Super-Twisting Algorithm (STA) which is able to ensure robustness...

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Veröffentlicht in:Journal of the Franklin Institute 2012-03, Vol.349 (2), p.685-699
Hauptverfasser: Derafa, L., Benallegue, A., Fridman, L.
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Fridman, L.
description This paper deals with the design and implementation of a nonlinear control algorithm for the attitude tracking of a four-rotor helicopter known as quadrotor. This algorithm is based on the second order sliding mode technique known as Super-Twisting Algorithm (STA) which is able to ensure robustness with respect to bounded external disturbances. In order to show the effectiveness of the proposed controller, experimental tests were carried out on a real quadrotor. The obtained results show the good performance of the proposed controller in terms of stabilization, tracking and robustness with respect to external disturbances.
doi_str_mv 10.1016/j.jfranklin.2011.10.011
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subjects Adaptative systems
Algorithms
Applied sciences
Computer science
control theory
systems
Control theory
Control theory. Systems
Disturbances
Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Mathematical analysis
Physics
Robustness
Solid dynamics (ballistics, collision, multibody system, stabilization...)
Solid mechanics
Stabilization
Tracking
Twisting
title Super twisting control algorithm for the attitude tracking of a four rotors UAV
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