Quadrotor Trajectory Tracking Control against Uncertainties for Autonomous Landing Task

被引:0
作者
Lee, Ji-Won [1 ]
Anh Tung Nguyen [1 ]
Nguyen Xuan-Mung [1 ]
Hong, Sung-Kyung [1 ]
机构
[1] Sejong Univ, Fac Mech & Aerosp Engn, Seoul 05006, South Korea
来源
2019 19TH INTERNATIONAL CONFERENCE ON CONTROL, AUTOMATION AND SYSTEMS (ICCAS 2019) | 2019年
关键词
Quadrotor; Landing; Tracking control; Backstepping; Time delay control; Switching action;
D O I
10.23919/iccas47443.2019.8971758
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The trajectory tracking control problem of quadrotor unmanned aerial vehicles has attracted great attention from researchers all around the world in recent years. Nevertheless, designing superior controllers for a quadrotor is still a challenge as model uncertainties, and external disturbances always exist and induce significant degradation in the control performance. In this paper, we propose two control laws to solve the quadrotor trajectory tracking and landing control problem under the presence of both uncertainties and external disturbances. Based on the backstepping control technique, the quadrotor attitude and the horizontal position controllers are devised to deal with the additive disturbances. In addition, the vertical position is controlled by a time-delay controller with switching action to address both additive and multiplicative uncertainties such as the system's mass-varying problem or the ground effect. Numerical simulation results demonstrate the effectiveness of the proposed algorithm.
引用
收藏
页码:55 / 60
页数:6
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