Embedded Super Twisting Control for the Attitude of a Quadrotor

被引:11
|
作者
Escobar, A. G. [1 ]
Alazki, H. [2 ]
Valenzuela, J. E. [1 ]
Garcia, O. [1 ]
机构
[1] CIIIA FIME UANL, Aerosp Engn Res & Innovat Ctr, Monterrey, Nuevo Leon, Mexico
[2] Autonomous Univ Ciudad Carmen, Fac Engn, Campeche, Mexico
关键词
Quadrotor; Embedded Control; Embedded Super Twisting Control; Sliding Mode Control; Flight Computer; 4; ROTORS; STABILIZATION;
D O I
10.1109/TLA.2016.7785921
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This paper focuses on the embedded Super Twisting control for the orientation dynamics of a quadrotor. The Newton-Euler approach is applied to obtain the dynamic model of the quadrotor and a functional description of the experimental platform is described. In order to implement the control algorithm and perform real-time flights, a commercial flight computer is used. Experimental results are obtained in real-time during the autonomous flight.
引用
收藏
页码:3974 / 3979
页数:6
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