首页 | 本学科首页   官方微博 | 高级检索  
     检索      

基于Leader-Follower的多无人机编队轨迹跟踪设计
引用本文:王晶,顾维博,窦立亚.基于Leader-Follower的多无人机编队轨迹跟踪设计[J].航空学报,2020,41(z1):723758-723758.
作者姓名:王晶  顾维博  窦立亚
作者单位:北京化工大学 信息科学与技术学院, 北京 100013
基金项目:北京市自然科学基金;国家自然科学基金;中央高校基本科研业务费专项基金
摘    要:针对四旋翼无人机(UAV)群在轨迹跟踪过程中易受外界干扰而引起跟踪误差的问题,设计了基于Leader-Follower的多无人机协同编队轨迹跟踪控制方法。在该系统中,首先通过积分反步法(IBS)对所建四旋翼飞行器模型设计Leader无人机的轨迹跟踪控制器。其次设计了滑模控制(SMC)器,以控制Leader与Follower无人机实现期望的编队队形并同时跟踪参考轨迹。然后通过数值仿真验证了算法的有效性,仿真结果表明,系统具有良好的控制精度。最后通过视觉定位系统进行实验,结果表明所设计的控制器能够实现多个无人机轨迹跟踪和编队控制,所设计的算法具有可行性。

关 键 词:积分反步法  滑模控制器  轨迹跟踪  编队控制  飞行实验  
收稿时间:2019-12-13
修稿时间:2019-12-25

Leader-Follower formation control of multiple UAVs with trajectory tracking design
WANG Jing,GU Weibo,DOU Liya.Leader-Follower formation control of multiple UAVs with trajectory tracking design[J].Acta Aeronautica et Astronautica Sinica,2020,41(z1):723758-723758.
Authors:WANG Jing  GU Weibo  DOU Liya
Institution:School of Information Science and Technology, Beijing University of Chemical Technology, Beijing 100013, China
Abstract:Leader-follower formation control of multiple Unmanned Aerial Vehicle (UAVs) is studied to solve the tracking error caused by the unknown disturbance on the quadrotor UAV group. In this system, firstly, the trajectory tracking controller of the leader UAV is designed by Integral BackStepping (IBS) on the established quadrotor aircraft model. Secondly, a formation control law based on Sliding Mode Control (SMC) is designed to drive the leader and follower UAVs to the desired formation while tracking the reference trajectory. Then the effectiveness of the designed control algorithms is verified by numerical simulations. The simulation results show that the system has good control accuracy. Finally, a experiment of the designed controllers is carried out on Parrot Bebop 2 quadrotor UAVs through the visual positioning system. The experimental results show that the designed controller can achieve the desired tracking and formation of multiple UAVs, verifying the feasibility of the designed controllers.
Keywords:integral backstepping  sliding mode controller  trajectory tracking  formation control  flight experiment  
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》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