To track the reference attitude angles and angular accelerations in the presence of strong uncertainties and disturbances, a new robust generalized predictive control (GPC) law is presented for a near-space hypersonic vehicle (NHV). The control law consists of the optimal GPC law and radius basis function disturbance observer (RBFDO). The output prediction defined on finite horizon is carried out via Taylor series expansion. The unmodeled dynamics and unknown disturbances in flight are estimated by the RBFDO, and the stability analysis of the close-loop system is provided also. The robust GPC law of the NHV proves to be able to attain the optimal index in mathematics. The simulation results show satisfactory performance of the presented controller for entry attitude tracking control, and the robustness to parameters variations and the disturbance rejection are successfully accomplished.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Attitude tracking of a near-space hypersonic vehicle using robust predictive control


    Contributors:
    Yanli Du, (author) / Qingxian Wu, (author) / Changsheng Jiang, (author) / Jie Wen, (author)


    Publication date :

    2008-12-01


    Size :

    669720 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Robust attitude predictive control design for hypersonic vehicles with state constraints

    Xingjie, Niu / Jianguo, Guo / Jun, Zhou et al. | SAGE Publications | 2019


    Robust Model Predictive Control for Attitude Control Tracking

    Chai, Runqi / Chen, Kaiyuan / Cui, Lingguo et al. | Springer Verlag | 2023



    Attitude control of unmanned hypersonic test vehicle

    Xin Wang, / Dongzhu Feng, / Yi Lin, | IEEE | 2008