DocumentCode :
184017
Title :
Attitude tracking control of a quadrotor based on absolutely continuous fractional integral sliding modes
Author :
Munoz-Vazquez, Aldo-Jonathan ; Parra-Vega, Vicente ; Sanchez-Orta, Anand ; Garcia, O. ; Izaguirre-Espinoza, Carlos
Author_Institution :
Robot. & Adv. Manuf. Div., Res. Center for Adv. Studies (Cinvestav), Saltillo, Mexico
fYear :
2014
fDate :
8-10 Oct. 2014
Firstpage :
717
Lastpage :
722
Abstract :
The model-free sliding mode control based on fractional order sliding surface is built upon: i) An absolutely continuous control structure that does not require the exact dynamic model to induce a fractional sliding motion in finite time, and ii) A methodology to design fractional references with a clear counterpart in the frequency domain is proposed. This in order to improve the system response, in particular the transient period, and to generate a high-performance during the sliding motion. Numerical simulations support the proposal and illustrates the closed-loop system, which provides a better insight of the proposed scheme.
Keywords :
attitude control; closed loop systems; frequency-domain analysis; helicopters; numerical analysis; variable structure systems; absolutely continuous control structure; absolutely continuous fractional integral sliding modes; closed-loop system; exact dynamic model; fractional order sliding surface; fractional sliding motion; model-free sliding mode control; numerical simulations; quadrotor attitude tracking control; Attitude control; Frequency-domain analysis; Laplace equations; Manifolds; Robots; Sliding mode control; Transient analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Applications (CCA), 2014 IEEE Conference on
Conference_Location :
Juan Les Antibes
Type :
conf
DOI :
10.1109/CCA.2014.6981425
Filename :
6981425
Link To Document :
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