Attitude constrained control of quadrotor unmanned aerial vehicle based on compensation function observer

被引:0
|
作者
Qi G.-Y. [1 ]
Li K. [1 ]
Wang K. [1 ]
机构
[1] Tianjin Key Laboratory of Intelligent Control of Electrical Equipment, Tiangong University, Tianjin
关键词
backstepping control; barrier Lyapunov function; compensation function observer(CFO); control theory and control engineering; extend state observer(ESO);
D O I
10.13229/j.cnki.jdxbgxb20220612
中图分类号
学科分类号
摘要
Due to the limitation of the flight environment of the quadrotor UAV and its own actuator,its attitude is often subject to various constraints. To ensure that the attitude always changes within the constraint range,the barrier Lyapunov function(BLF)was introduced to ensure that the attitude always varies within the constraint range to ensure that the system can achieve the preset performance. A compensation function observer based BLF attitude constrained backstepping control(CFO-BLF)scheme was proposed. Simulink simulation compares the CFO-BLF backstepping control, ESO-BLF backstepping control and PID control algorithms by testing the attitude tracking performance of the quadrotor UAV to verify the effectiveness and superiority of CFO-BLF. © 2023 Editorial Board of Jilin University. All rights reserved.
引用
收藏
页码:853 / 862
页数:9
相关论文
共 50 条
  • [21] Robust image-based control of the quadrotor unmanned aerial vehicle
    Asl, Hamed Jabbari
    Yoon, Jungwon
    [J]. NONLINEAR DYNAMICS, 2016, 85 (03) : 2035 - 2048
  • [22] Exact linearization and sliding mode observer for a quadrotor unmanned aerial vehicle
    Mokhtari, A.
    Benallegue, A.
    Orlov, Y.
    [J]. International Journal of Robotics and Automation, 2006, 21 (01): : 39 - 49
  • [23] Pose Control of Quadrotor Unmanned Aerial Vehicle Based on Double Filters
    Zhang, Yunzhou
    Zhang, Yihan
    Mu, Xiang
    Wang, Yuxi
    [J]. 2015 IEEE INTERNATIONAL CONFERENCE ON CYBER TECHNOLOGY IN AUTOMATION, CONTROL, AND INTELLIGENT SYSTEMS (CYBER), 2015, : 298 - 304
  • [24] Exact linearization and sliding mode observer for a quadrotor unmanned aerial vehicle
    Mokhtari, A
    Benallegue, A
    Orlov, Y
    [J]. INTERNATIONAL JOURNAL OF ROBOTICS & AUTOMATION, 2006, 21 (01): : 39 - 49
  • [25] Autonomous Control System for the Quadrotor Unmanned Aerial Vehicle
    Zhang Yao
    Xian Bin
    Yin Qiang
    Liu Yang
    Wang Fu
    [J]. PROCEEDINGS OF THE 31ST CHINESE CONTROL CONFERENCE, 2012, : 4862 - 4867
  • [26] Autonomous Hovering Control for a Quadrotor Unmanned Aerial Vehicle
    Wang Fu
    Xian Bin
    Huang Guoping
    Zhao Bo
    [J]. 2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 620 - 625
  • [27] Integral sliding mode control method for quadrotor unmanned aerial vehicle based on finite-time observer
    Zhu W.
    Wang L.
    Tian B.
    [J]. Zhongguo Guanxing Jishu Xuebao/Journal of Chinese Inertial Technology, 2023, 31 (12): : 1244 - 1253
  • [28] Autonomous control system for the quadrotor unmanned aerial vehicle
    Wei, Xiaojuan
    [J]. 2016 13TH INTERNATIONAL CONFERENCE ON UBIQUITOUS ROBOTS AND AMBIENT INTELLIGENCE (URAI), 2016, : 796 - 799
  • [29] Tracking Control Design for Quadrotor Unmanned Aerial Vehicle
    Nadda, Sudhir
    Swarup, A.
    [J]. DEFENCE SCIENCE JOURNAL, 2017, 67 (03) : 245 - 253
  • [30] Sliding Mode Attitude Control for a Quadrotor Micro Unmanned Aircraft Vehicle Using Disturbance Observer
    Wang, Honglin
    Chen, Mou
    [J]. 2014 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2014, : 568 - 573