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首页|期刊导航|南京航空航天大学学报|基于ORB的交叉双旋翼无人直升机视觉跟踪控制系统

基于ORB的交叉双旋翼无人直升机视觉跟踪控制系统

席鹏航 李京阳 印明威 杨洪伟 宝音贺西

南京航空航天大学学报2023,Vol.55Issue(6):966-976,11.
南京航空航天大学学报2023,Vol.55Issue(6):966-976,11.DOI:10.16356/j.1005-2615.2023.06.003

基于ORB的交叉双旋翼无人直升机视觉跟踪控制系统

A Visual Tracking Control System for Intermeshing-Rotor Unmanned Helicopters Based on ORB

席鹏航 1李京阳 2印明威 3杨洪伟 4宝音贺西5

作者信息

  • 1. 天津工业大学机械工程学院,天津 300387
  • 2. 天津工业大学机械工程学院,天津 300387||中北大学航空宇航学院,太原 030051
  • 3. 北京清航紫荆装备科技有限公司,北京 102101
  • 4. 南京航空航天大学航天学院,南京 211106
  • 5. 清华大学航空航天学院,北京 100084||内蒙古工业大学航空学院,呼和浩特 010051
  • 折叠

摘要

Abstract

To enable visual tracking of targets by intermeshing-rotor unmanned helicopters in the presence of unstable global positioning system(GPS)signals,a visual tracking control system for intermeshing-rotor unmanned helicopters is designed.Firstly,a vision module is designed to perform image processing on tracked targets,obtain the pixel coordinates of the center point of the tracked target using oriented FAST and rotated BRIEF(ORB)feature matching and rectangle detection.Thus,the actual position of the center point of the tracked target is solved by the camera model and the rotation matrix.Secondly,a tracking control module is designed with a serial proportional-integral-derivative(PID)plus feed-forward control structure.An open-square controller is used in the position control in order to limit the limit position and maximum acceleration,and an intermeshing-rotor attitude control mechanism is designed in the attitude control.Then,the simulation environment is built by the flight control ground station to simulate and verify the flight control system with the added vision module.The results show that the unmanned helicopter can track the desired position output from the vision module very well.Finally,the experimental validation is conducted under the conditions of the maximum flight speed of 1 m/s,the maximum attitude angle of about 8°,and the maximum error of 0.08 m between the position and the desired position.The experiment demonstrates that the proposed system can fulfill the visual tracking of the intermeshing-rotor unmanned helicopter for the target.

关键词

交叉双旋翼无人直升机/视觉跟踪/特征匹配/位置控制/姿态控制

Key words

intermeshing-rotor unmanned helicopter/visual tracking/feature matching/position control/attitude control

分类

航空航天

引用本文复制引用

席鹏航,李京阳,印明威,杨洪伟,宝音贺西..基于ORB的交叉双旋翼无人直升机视觉跟踪控制系统[J].南京航空航天大学学报,2023,55(6):966-976,11.

基金项目

国家自然科学基金(11602123) (11602123)

内蒙古自治区杰出青年培育基金(2019JQ002). (2019JQ002)

南京航空航天大学学报

OA北大核心CSCDCSTPCD

1005-2615

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