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小型无人直升机航向线性自抗扰控制

丁力 马瑞 单文桃 吴洪涛

农业机械学报2017,Vol.48Issue(5):22-27,6.
农业机械学报2017,Vol.48Issue(5):22-27,6.DOI:10.6041/j.issn.1000-1298.2017.05.002

小型无人直升机航向线性自抗扰控制

Linear Active Disturbance Rejection Control for Yaw Channel of Small-scale Unmanned Helicopter

丁力 1马瑞 2单文桃 3吴洪涛1

作者信息

  • 1. 江苏理工学院机械工程学院,常州 213001
  • 2. 南洋理工大学机械与宇航工程学院,新加坡 639798
  • 3. 南京航空航天大学机电学院,南京 210016
  • 折叠

摘要

Abstract

Small-scale unmanned helicopter has a peculiar flight feature of vertically take-off and landing,fixed position hovering,flying in low velocity,forward flight,rearward flight and so on.It is mainly used for civilian and military field with the advantage of light weight,low price and small scale.However,the small-scale unmanned helicopter is a strong coupled,under actuated,multivariable,time varying,open-loop unstable and high order nonlinear system.It is a great challenge to realize the research of its autonomous flight.Aiming at the internal uncertainties and large disturbance of the small-scale unmanned helicopter,a controller for yaw channel based on linear active disturbance rejection controller (LADRC) was proposed to realize the high performance control.Firstly,the yaw model of Trex-600 unmanned helicopter was analyzed and deduced,and the gust model was introduced to simulate the actual flight environment.Then,the principle of LADRC was elaborated and the yaw control system was designed based on LADRC of second order.In order to obtain the appropriate control parameters,the novel artificial bee colony algorithm was applied to conduct parameters tuning.Lastly,a trajectory tracking simulation and experiment were used to test the proposed controller compared with the PID controller.The results showed that the LADRC controller had the ability of good robustness,fast response and high control precision.The yaw angle of the Trex-600 unmanned helicopter can track the referenced trajectory fleetly and accurately.

关键词

小型无人直升机/线性自抗扰控制/人工蜂群算法/参数整定/轨迹跟踪

Key words

small-scale unmanned helicopter/linear active disturbance rejection control/artificial bee colony algorithm/parameters tuning/trajectory tracking

分类

信息技术与安全科学

引用本文复制引用

丁力,马瑞,单文桃,吴洪涛..小型无人直升机航向线性自抗扰控制[J].农业机械学报,2017,48(5):22-27,6.

基金项目

国家自然科学基金青年基金项目(51405209) (51405209)

农业机械学报

OA北大核心CSCDCSTPCD

1000-1298

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