Height and attitude active disturbance rejection controller design of a small-scale helicopter

被引:0
|
作者
Shuai Tang
QiuHui Yang
ShaoKe Qian
ZhiQiang Zheng
机构
[1] National University of Defense Technology,College of Mechatronic Engineering and Automation
来源
关键词
small-scale helicopter; active disturbance rejection control (ADRC); extended state observer (ESO); backstepping; disturbance compensation; 032202;
D O I
暂无
中图分类号
学科分类号
摘要
Small-scale helicopters are very attractive because of their unique features. However, autonomous flight control for small-scale helicopters is still a challenging work because they are naturally unstable, strongly nonlinear, and sensitive to disturbances. In this paper, we focus on the design of a height and attitude active disturbance rejection controller (ADRC) for a small-scale helicopter constructed in our lab. Firstly, a comprehensive nonlinear model for the platform is presented, which is obtained through first principles modeling and system identification. The controller is designed using backstepping technique incorporated with extended state observer (ESO), which is used to estimate the unknown disturbances. Then, the estimate is introduced into the control law to compensate for the disturbances. The design specifications of military rotorcraft are introduced to guide the controller design to achieve specified control performance. Considering the physical limitations, reference models are designed to shape the desired control responses. At last, several flight simulations are carried out to validate the effectiveness and robustness of the proposed controller. The results show that the proposed controller works well and Level 1 performance can be achieved.
引用
收藏
页码:1 / 17
页数:16
相关论文
共 50 条
  • [1] Height and attitude active disturbance rejection controller design of a small-scale helicopter
    TANG Shuai
    YANG QiuHui
    QIAN ShaoKe
    ZHENG ZhiQiang
    [J]. Science China(Information Sciences), 2015, 58 (03) : 142 - 158
  • [2] Height and attitude active disturbance rejection controller design of a small-scale helicopter
    Tang Shuai
    Yang QiuHui
    Qian ShaoKe
    Zheng ZhiQiang
    [J]. SCIENCE CHINA-INFORMATION SCIENCES, 2015, 58 (03) : 1 - 17
  • [3] Sliding mode attitude controller design of a small-scale helicopter
    Zhou, Bin
    Tang, Shuai
    Li, Peng
    Zheng, Zhiqiang
    [J]. 26TH CHINESE CONTROL AND DECISION CONFERENCE (2014 CCDC), 2014, : 2441 - 2446
  • [4] Active Disturbance Rejection Control Design of the Yaw Channel for a Small-scale Helicopter based on Backstepping
    Tang, Shuai
    Mao, Longbo
    Liu, Guosong
    Wang, Weijun
    [J]. PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 8073 - 8078
  • [5] Adaptive Height and Attitude Control of Small-scale Unmanned helicopter
    Tang, Shuai
    Zhang, Li
    Zheng, ZhiQiang
    [J]. 2013 25TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2013, : 1 - 6
  • [6] Second-order sliding mode attitude controller design of a small-scale helicopter
    Tang, Shuai
    Zhang, Li
    Qian, Shaoke
    Zheng, Zhiqiang
    [J]. SCIENCE CHINA-INFORMATION SCIENCES, 2016, 59 (11)
  • [7] Second-order sliding mode attitude controller design of a small-scale helicopter
    Shuai TANG
    Li ZHANG
    Shaoke QIAN
    Zhiqiang ZHENG
    [J]. Science China(Information Sciences), 2016, 59 (11) : 128 - 141
  • [8] Active disturbance rejection controller design for spacecraft attitude maneuver
    Zhou, Li-Ni
    Tang, Guo-Jin
    Li, Hai-Yang
    [J]. Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics, 2007, 29 (12): : 2122 - 2126
  • [9] Robust controller design of small-scale unmanned helicopter
    Liu, Pei-zhi
    Bai, Zhi-qiang
    Wang, Jin-hua
    [J]. INTERNATIONAL JOURNAL OF MODELLING IDENTIFICATION AND CONTROL, 2011, 12 (1-2) : 17 - 21
  • [10] An Intelligence Attitude Controller Based on Active Disturbance Rejection Control Technology for an Unmanned Helicopter
    Shen, Suiyuan
    Xu, Jinfa
    Chen, Pei
    Xia, Qingyuan
    [J]. IEEE TRANSACTIONS ON VEHICULAR TECHNOLOGY, 2023, 72 (03) : 2936 - 2946