Real-time altitude control for a quadrotor helicopter using a super-twisting controller based on high-order sliding mode observer

被引:24
作者
Gonzalez-Hernandez, Ivan [1 ]
Munoz Palacios, Filiberto [2 ,3 ]
Salazar Cruz, Sergio [1 ]
Espinoza Quesada, Eduardo Steed [3 ]
Lozano Leal, Rogelio [1 ]
机构
[1] CINVESTAV, UMI LAFMIA CNRS 3175, French Mexican Lab Comp Sci & Automat, Mexico City, DF, Mexico
[2] CINVESTAV, Dept Automat Control, Mexico City, DF, Mexico
[3] Polytech Univ Pachuca, Dept Mechatron, Zempoala 43830, Hidalgo, Mexico
关键词
Super-twisting controller; high-order sliding mode observer; quadrotor helicopter; ATTITUDE;
D O I
10.1177/1729881416687113
中图分类号
TP24 [机器人技术];
学科分类号
080202 ; 1405 ;
摘要
This article addresses the problem of altitude tracking for unmanned aircraft system when the altitude velocity is unknown, because in a practical implementation, the available sensors used to measure the vehicle's altitude (barometer, global positioning system, laser, etc.) do not provide the altitude velocity. We propose a control strategy based on both the super-twisting sliding mode controller as well as a high-order sliding mode observer to control and to estimate the altitude velocity, respectively. A comprehensive stability analysis for the combined controller-observer based on the Lyapunov stability theory is presented, ensuring the asymptotic convergence of the tracking error under external bounded disturbances. To demonstrate the performance and the effectiveness of the proposed solution, an extensive set of real-time experimental tests performed at outdoor environments is presented.
引用
收藏
页数:15
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