Attitude control for micro-vehicle based on fuzzy adaptive algorithm

被引:0
|
作者
Dept. of Automation Engineering, Northeastern Univ. Qinhuangdao Branch, Qinhuangdao 066004, China [1 ]
不详 [2 ]
机构
来源
关键词
Robustness (control systems) - Computation theory - Uncertainty analysis - Adaptive control systems - Nonlinear systems - Adaptive algorithms - Robust control - Vehicles;
D O I
暂无
中图分类号
学科分类号
摘要
A fuzzy adaptive control algorithm for a class of uncertain nonlinear systems based on Lyapunov's stability theory is proposed. The main idea of the algorithm is that the system is divided into a nominal model and the lumped disturbance terms, which are composed of modeling error, parameter uncertainties, disturbances and unmodeled dynamics. Fuzzy adaptive control is adopted to approach every uncertain parameter of the system in real time, and robust feedback control is introduced to eliminate the external disturbances. Resultingly, every uncertain parameter of the input coefficient matrix and the function vector in the system is approached. The control precision and robustness are improved, the on-line computation is decreased correspondingly, and the output of the nonlinear system is tracked gradually. The stability is proved and the algorithm is applied to the attitude control of a micro-vehicle. The simulation result verifies the effectiveness of the proposed method.
引用
收藏
相关论文
共 50 条
  • [21] Attitude Control of a Robot in Sewer Pipe Based on Fuzzy Algorithm
    Yang Qingmei
    Chi Xiaozhu
    PROCEEDINGS OF THE 29TH CHINESE CONTROL CONFERENCE, 2010, : 2645 - 2648
  • [22] Analysis on driving stability of micro-vehicle based on human-seat dynamics system
    Shu, Hongyu
    Luo, Shuang
    Yao, Zejie
    INTERNATIONAL JOURNAL OF VEHICLE DESIGN, 2018, 77 (04) : 272 - 285
  • [23] Characteristic model-based adaptive attitude control for hypersonic vehicle
    Gong Y.-L.
    Wu H.-X.
    Yuhang Xuebao/Journal of Astronautics, 2010, 31 (09): : 2122 - 2128
  • [24] The Nonlinear Adaptive Attitude Control for Hypersonic Vehicle
    Hu J.
    Hu, Jun (hujunbice@126.com), 1600, China Spaceflight Society (38): : 1281 - 1288
  • [25] Fuzzy Sliding Mode Control for Attitude of Flapping Wing Micro Aerial Vehicle Based on Variable Rate Reaching Law
    Hu, Shengbin
    Lu, Wenhua
    Chen, Zhiyi
    Lei, Lei
    Zhang, Yixuan
    SUSTAINABLE ENVIRONMENT AND TRANSPORTATION, PTS 1-4, 2012, 178-181 : 2801 - 2804
  • [26] Flapping Wing Micro Aerial Vehicle Attitude Control with Fuzzy Sliding Mode Controller Based on RBF Neural Network
    Hu, Shengbin
    Lu, Wenhua
    Lu, Minxun
    MANUFACTURING SCIENCE AND MATERIALS ENGINEERING, PTS 1 AND 2, 2012, 443-444 : 177 - +
  • [27] Adaptive Fuzzy DSC Control Based on ISpS for Hypersonic Vehicle
    Hu, Chaofang
    Liu, Yanwen
    2013 25TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2013, : 430 - 435
  • [28] Simulation research on hypersonic vehicle based on fuzzy adaptive control
    Zhu, Zhouli
    Chen, Wei
    Zhou, Wei
    Li, Qun
    PROCEEDINGS OF THE 2ND INTERNATIONAL CONFERENCE ON COMPUTER ENGINEERING, INFORMATION SCIENCE & APPLICATION TECHNOLOGY (ICCIA 2017), 2017, 74 : 186 - 192
  • [29] Simulation of Vehicle ESP Based on Adaptive Fuzzy PID Control
    Wan, Neng
    Zeng, Guangping
    Zhang, Chunguang
    Luo, Yating
    2020 12TH INTERNATIONAL CONFERENCE ON ADVANCED COMPUTATIONAL INTELLIGENCE (ICACI), 2020, : 310 - 315
  • [30] The Direct Adaptive Fuzzy Control for Satellite Attitude Control
    Guan, Ping
    Zhang, Wei
    Liu, Xiao-he
    Li, Ming-hui
    2011 CHINESE CONTROL AND DECISION CONFERENCE, VOLS 1-6, 2011, : 2185 - 2190