首页 | 本学科首页   官方微博 | 高级检索  
     

多旋翼无人机自主精准降落的控制系统研究
引用本文:曾振华,郑汇峰,祝玉杰,罗志勇. 多旋翼无人机自主精准降落的控制系统研究[J]. 广东工业大学学报, 2020, 37(1): 87-94. DOI: 10.12052/gdutxb.190102
作者姓名:曾振华  郑汇峰  祝玉杰  罗志勇
作者单位:1. 广东工业大学 自动化学院, 广东 广州 510006;2. 广州优飞信息科技有限公司, 广东 广州 510006
基金项目:广东省自然科学基金资助项目(2018A0303130137);广东省哲学社会科学规划学科共建项目(GD18XJY05);广东省高性能计算重点实验室开放项目(TH1528);深圳市南山区科技计划项目(2018050)
摘    要:针对多旋翼无人机降落时采用位置控制方式存在位置振荡和速度超调现象的问题,本文采用速度控制的方式进行降落,构建了一个完整的精准降落闭环速度控制系统。首先建立无人机精准降落速度控制系统的总体框架;然后进行无人机降落时多个坐标系之间的转换;再设计外环速度的"比例-积分-微分"(Proportion-Integral-Derivative,PID)控制系统和模糊自适应速度PID控制系统;最后进行2种控制系统的性能测试和对比实验。结果表明,无人机在这2种控制系统下均能成功降落到地面靶标上,且模糊自适应速度PID控制系统降落精度更高,达到了0.13 m以内。因此多旋翼无人机采用模糊自适应速度PID控制系统可实现自主精准降落。

关 键 词:多旋翼无人机  模糊自适应  PID控制  闭环  精准降落  
收稿时间:2019-08-09

A Research on Control System of Multi-rotor UAV Self-precision Landing
Zeng Zhen-hua,Zheng Hui-feng,Zhu Yu-Jie,Luo Zhi-Yong. A Research on Control System of Multi-rotor UAV Self-precision Landing[J]. Journal of Guangdong University of Technology, 2020, 37(1): 87-94. DOI: 10.12052/gdutxb.190102
Authors:Zeng Zhen-hua  Zheng Hui-feng  Zhu Yu-Jie  Luo Zhi-Yong
Affiliation:1. School of Automation, Guangdong University of Technology, Guangzhou 510006, China;2. Guangzhou Ufly Information Technology Co., Ltd., Guangzhou 510006, China
Abstract:In view of the problem of positional oscillation and speed overshoot in the position control mode of multi-rotor UAV landing, the speed control method is adopted to land and a complete closed-loop speed control system constructed for precise landing. Firstly, the overall framework of UAV precise landing speed control system is established; secondly, the coordinate system of UAV landing and the transformation between coordinate systems are constructed; then, the outer-loop speed PID(Proportion-Integral-Derivative) control system and the fuzzy adaptive speed PID control system are designed; and finally, the performance tests and comparative experiments of the two control systems are carried out. The results show that the UAV can successfully land on the ground target under these two control systems, and the fuzzy adaptive speed PID control system has a higher landing accuracy, which is less than 0.13 meters. It can be seen that the multi-rotor UAV has realized the autonomous precise landing by adopting the fuzzy adaptive speed PID control system.
Keywords:multi-rotor UAV  fuzzy adaptive  PID control  closed-loop  precise landing  
点击此处可从《广东工业大学学报》浏览原始摘要信息
点击此处可从《广东工业大学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号