Quadcopter Precision Landing on Moving Targets via Disturbance Observer-Based Controller and Autonomous Landing Planner

被引:12
|
作者
Nguyen Xuan-Mung [1 ]
Ngoc Phi Nguyen [1 ]
Tan Nguyen [2 ]
Dinh Ba Pham [3 ]
Mai The Vu [4 ]
Ha Le Nhu Ngoc Thanh [5 ]
Hong, Sung Kyung [1 ,6 ]
机构
[1] Sejong Univ, Dept Aerosp Engn, Seoul 05006, South Korea
[2] Dong Nai Technol Univ, Dept Technol, Bien Hoa 810000, Vietnam
[3] Vietnam Maritime Univ, Dept Mech Engn, Haiphong 180000, Vietnam
[4] Sejong Univ, Sch Intelligent Mechatron Engn, Seoul 05006, South Korea
[5] Ho Chi Minh City Univ Technol & Educ, Dept Mechatron Engn, Ho Chi Minh City 71307, Vietnam
[6] Sejong Univ, Dept Convergence Engn Intelligent Drone, Seoul 05006, South Korea
基金
新加坡国家研究基金会;
关键词
Cameras; Visualization; Vehicle dynamics; Heuristic algorithms; Urban areas; Global Positioning System; Autonomous aerial vehicles; Autonomous vehicle; quadcopter; unmanned aerial vehicle; precision landing; moving target; disturbance observer; robust control; mission planing; QUADROTOR; STRATEGY; VEHICLE; FLIGHT; UAVS;
D O I
10.1109/ACCESS.2022.3197181
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Unmanned aerial vehicles, especially quadcopters, play key roles in many real-world applications and the related quadcopter autonomous control algorithms have attracted a great deal of attention. In this paper, we address the vision-based autonomous landing problem of a quadcopter on a ground moving target. Firstly, we propose a disturbance observer-based control algorithm, consisting of a nonlinear disturbance observer and robust altitude and attitude controllers. This algorithm is based on the quadcopter dynamics model, and its stability is strictly proved using Lyapunov's theory. Secondly, we develop an autonomous landing planner which we test for various landing scenarios to deliver improved reliability and accuracy of the landing mission. These theoretical studies are complemented by a numerical feasibility study, before demonstrating the effectiveness of our approach under actual flight conditions with an experimental quadcopter platform.
引用
收藏
页码:83580 / 83590
页数:11
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