On Modified ADRC Design for Uncertain Systems Under Actuator Dynamics of Limited Bandwidth With Application to 2-DOF Helicopters

被引:0
作者
Xiang, Feiyu [1 ,2 ]
Xue, Wenchao [1 ,2 ]
Chen, Sen [3 ]
Li, Miao [3 ]
机构
[1] Chinese Acad Sci, Acad Math & Syst Sci, NCMIS, LSC, Beijing 100190, Peoples R China
[2] Univ Chinese Acad Sci, Sch Math Sci, Beijing 100049, Peoples R China
[3] Shaanxi Normal Univ, Sch Math & Stat, Xian 710119, Peoples R China
基金
中国国家自然科学基金;
关键词
Actuators; Aerodynamics; Bandwidth; Uncertainty; Vectors; Uncertain systems; Trajectory; Active disturbance rejection control (ADRC); actuator dynamics; extended state observer (ESO); Quanser Aero 2-DOF helicopter; uncertain systems; DISTURBANCE REJECTION CONTROL; OBSERVER; TRACKING; ENGINE; MOTOR;
D O I
10.1109/TIE.2024.3426047
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
In this article, the control problem for a class of uncertain systems under limited actuator dynamics is considered. A new modified active disturbance rejection control (ADRC) design is proposed to deal with external disturbance and unmodelled uncertainties despite actuator dynamics with limited bandwidth. First, it is shown that the traditional ADRC may lead to instability of the closed-loop system under actuator dynamics of limited bandwidth. Second, the tracking error between the system state vectors and the desired trajectory under the proposed ADRC is rigorously analyzed for transient and steady performance. It is proven that the tracking error can converge to the desired region by tuning the parameters of the extended state observer (ESO) under the bandwidth in actuator dynamics. Finally, the proposed method is applied to a Quanser Aero two-degree-of-freedom (2-DOF) helicopter with external disturbance and unmodelled dynamics. The experimental results show the superiority of our method over traditional ADRC.
引用
收藏
页码:1980 / 1989
页数:10
相关论文
共 32 条
  • [1] Inverted decoupling and LMI-based controller design for a turboprop engine with actuator dynamics
    Chen, Huairong
    Wang, Xi
    Wang, Haonan
    Gu, Nannan
    Zhu, Meiyin
    Yang, Shubo
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (06) : 1774 - 1787
  • [2] A nonlinear disturbance observer for robotic manipulators
    Chen, WH
    Ballance, DJ
    Gawthrop, PJ
    O'Reilly, J
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2000, 47 (04) : 932 - 938
  • [3] Performance Recovery of Feedback-Linearization-Based Designs
    Freidovich, Leonid B.
    Khalil, Hassan K.
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2008, 53 (10) : 2324 - 2334
  • [4] Gao ZQ, 2003, P AMER CONTR CONF, P4989
  • [5] A New Quadratic Spacing Policy and Adaptive Fault-Tolerant Platooning With Actuator Saturation
    Guo, Ge
    Li, Ping
    Hao, Li-Ying
    [J]. IEEE TRANSACTIONS ON INTELLIGENT TRANSPORTATION SYSTEMS, 2022, 23 (02) : 1200 - 1212
  • [6] From PID to Active Disturbance Rejection Control
    Han, Jingqing
    [J]. IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2009, 56 (03) : 900 - 906
  • [7] Active disturbance rejection control: Methodology and theoretical analysis
    Huang, Yi
    Xue, Wenchao
    [J]. ISA TRANSACTIONS, 2014, 53 (04) : 963 - 976
  • [8] Active Disturbance Rejection Station-Keeping Control for Solar-Sail Libration-Point Orbits
    Lou, Zhangpeng
    Zhang, Kaitian
    Wang, Yong
    Gao, Qing
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2016, 39 (08) : 1913 - 1917
  • [9] Luo Y, 2004, P AMER CONTR CONF, P1695
  • [10] Control-oriented modeling of an air-breathing hypersonic vehicle
    Parker, Jason T.
    Serrani, Andrea
    Yurkovich, Stephen
    Bolender, Michael A.
    Doman, David B.
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (03) : 856 - 869