For the hypersonic vehicle nonlinear attitude mode in reentry process with a strong coupling, aerodynamic parameter perturbations and non-deterministic, combine extended state observer and nonlinear law state error feedback, design the hypersonic vehicle MIMO-ESO ADRC attitude controller. Put interference such as uncertainty, coupling and parameter perturbations as “the sum of interference” ,use the extended state observer to estimate and dynamic feedback compensation, use nonlinear law state error feedback to inhibit residual of compensation. ADRC controller is charged without a precise model of vehicle , and without precise perturbation boundaries of aerodynamic parameters.Simulation results show that the MIMO-ESO ADRC attitude controller can overcome the impact of large-scale perturbations of interference and aerodynamic parameters, have good dynamic qualities and tracking capabilities, also have strong robustness.


    Access

    Download


    Export, share and cite



    Title :

    ADRC Attitude Controller Design for Hypersonic Vehicle based on MIMO-ESO


    Contributors:
    Wen JianHua (author) / Qin ChangMao (author) / Zhang Xin (author)


    Publication date :

    2018




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Fault-Tolerant Integrated Guidance and Control Design for Hypersonic Vehicle Based on ADRC

    Yan, Guocheng / Wang, Honglun / Wu, Tiancai et al. | Springer Verlag | 2024


    Research on Attitude Control of Spacecraft Based on ADRC

    Teng, Fu Lin ;Ge, Hong Yu ;Li, Hong Sheng | Trans Tech Publications | 2011


    Attitude Control of Quadrotor UAV Based on ADRC

    Wang, Haoyu / Zhuo, Jiajin / Xiong, Xingjia | IEEE | 2023


    Adaptive control of missile attitude based on BP–ADRC

    Qiao, Haiyan / Meng, Hao / Ke, Wei et al. | Emerald Group Publishing | 2020


    Attitude Control of Underactuated Quadrotor UAV Based on Improved ADRC

    Wang, Chenyun / Xia, Yuanqing / Kong, Xiangyu et al. | IEEE | 2023