首页 | 本学科首页   官方微博 | 高级检索  
     

基于光流的四旋翼直升机鲁棒自主着陆控制
引用本文:张连华,王京,石宗英,钟宜生. 基于光流的四旋翼直升机鲁棒自主着陆控制[J]. 控制理论与应用, 2016, 33(11): 1492-1500
作者姓名:张连华  王京  石宗英  钟宜生
作者单位:中国航天员科研训练中心,清华大学自动化系,清华大学自动化系,清华大学自动化系
基金项目:国家自然科学基金项目(61374034, 61210012)资助.
摘    要:针对小型四旋翼无人机自主着陆问题,提出了一种基于光流的高度估计方法和基于信号补偿的高度鲁棒控制器设计方法.首先从通用光流运动模型出发,采用奇异值分解方法求解无人机线速度和深度的比值,通过对垂直速度和高度比值积分获得高度数据.其次,将考虑地效影响和其它不确定性的高度通道非线性模型分解为标称线性模型和等效扰动两部分,并设计基于信号补偿的高度鲁棒控制器,该控制器由标称控制器和鲁棒补偿器组成,其中标称控制器使得标称闭环系统达到期望的高度跟踪特性,鲁棒补偿器用于抑制等效扰动的影响.最后从理论上证明了该控制器可以保证高度跟踪误差在有限时间内收敛至指定的原点邻域内.四旋翼无人机自主着陆的实验结果验证了所提出的基于光流的高度估计和鲁棒控制方法的有效性.

关 键 词:无人机   光流   鲁棒控制   自主着陆
收稿时间:2016-01-26
修稿时间:2016-10-11

Robust autonomous landing control of quadrotor based on optical flow
ZHANG Lian-hu,WANG Jing,SHI Zong-ying and ZHONG Yi-sheng. Robust autonomous landing control of quadrotor based on optical flow[J]. Control Theory & Applications, 2016, 33(11): 1492-1500
Authors:ZHANG Lian-hu  WANG Jing  SHI Zong-ying  ZHONG Yi-sheng
Affiliation:China Astronaut Research and Training Center,Department of Automation, Tsinghua University,Department of Automation, Tsinghua University,Department of Automation, Tsinghua University
Abstract:For autonomous landing of a small quadrotor, an attitude estimation method is proposed using optical flow,and a robust controller based on signal compensation is designed. Firstly, the ratio of velocity to depth is acquired bysingular value decomposition (SVD) from the general optical flow motion model, and the altitude data are obtained byintegrating the ratio of vertical speed and altitude. Then, the nonlinear model of the altitude channel is divided into anominal linear model and an equivalent disturbance considering the influences of the ground effect and other uncertainties.And a robust controller based on signal compensation is designed, which consists of a nominal controller and a robustcompensator. The nominal controller is designed for the nominal system to get the desired tracking performance, and therobust compensator is applied to restrain the influence of the equivalent disturbance. Finally, it is proved that the trackingerror for the altitude channel can converge to a given neighborhood of the origin in finite time by the robust controller.Landing experimental results for a small quadrotor demonstrate the effectiveness of the proposed altitude estimation methodbased on optical flow and the robust controller.
Keywords:unmanned aerial vehicle   optical flow   robust control   automous landing
本文献已被 CNKI 等数据库收录!
点击此处可从《控制理论与应用》浏览原始摘要信息
点击此处可从《控制理论与应用》下载全文
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