Visual Servoing of a 3 DOF Hover Quadcopter using 2D Markers

被引:0
作者
Ouerdane, Fethi [1 ]
Mysorewala, Muhammad Faizan [1 ,2 ]
机构
[1] King Fahd Univ Petr & Minerals KFUPM, Dept Control & Instrumentat Engn, Interdisciplinary Res Ctr Smart Mobil & Logist, Dhahran 31261, Saudi Arabia
[2] King Fahd Univ Petr & Minerals KFUPM, Interdisciplinary Res Ctr Intelligent Mfg & Robot, Dhahran 31261, Saudi Arabia
来源
2024 33RD INTERNATIONAL SYMPOSIUM ON INDUSTRIAL ELECTRONICS, ISIE 2024 | 2024年
关键词
QR code; visual servoing; PID; LQR; control; Quadcopter; image processing;
D O I
10.1109/ISIE54533.2024.10595721
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
This study presents a novel approach for testing visual servoing on 3 DOF UAVs (Unmanned aerial vehicles) in an indoor environment with no GPS by employing a combination of a physical 3 DOF and simulating the rest of degrees, 2D markers are used to store instructions to previously known coordinates in the environment. Low-cost UAV hardware with an onboard camera can extract the task information from such markers without needing a ground station computer and continuous marker detection to follow a particular desired trajectory. Such a goal is achieved through the presence of markers, such as QR (Quick Response) codes, at selected locations, controlling the UAV motion to read and extract the stored information in the code, and controlling various states of UAV to fulfill the desired motion of moving through the site. This solution combines simulation and physical testing such that final algorithm can be applied on 6 DOF UAVs for asset monitoring and inspection in indoor environments, and non-experts can modify the vehicle's path by providing the QR codes. Experimental results for the centering of UAV for accurate QR code reading using PID (Proportional-Integral-Derivative) controller and LQR (Linear Quadratic Regulator) algorithm for attitude control are tested on Quanser's 3-DOF hover quadcopter in LabVIEW environment. Furthermore, hardware-in-the-loop simulation tests are performed to simulate the control of the linear motion of the UAV. The results achieved so far are promising and give ample encouragement to test and evaluate the technique on a 6-DOF UAV.
引用
收藏
页数:6
相关论文
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