The paper focuses on the problem of attitude control for hypersonic gliding vehicle (HGV) with unknown parameters. For near-space hypersonic gliding vehicle, the flight environment in reentry phase is very complex, and with the extremely high velocity, control of the aircraft is facing severe challenges. One of the challenges is that the exact values of the parameters in the kinetic model cannot be obtained. An observer-based approach is proposed in this paper to solve the problem and nonlinear dynamic inversion is used in controller design. Simulation on the longitudinal dynamic model of HGV presents the performance of the observer and the controller, which proved to be effective on this problem.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Observer-based attitude control for hypersonic gliding vehicle


    Contributors:
    Gao, Kehan (author) / Li, Qingdong (author) / Ren, Zhang (author) / Bai, Chen (author)


    Publication date :

    2014-08-01


    Size :

    112487 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Observer Based Fixed-Time Tracking Control for Hypersonic Gliding Vehicle

    Dong, Zhaorong / Zhao, Min / Jiang, Li et al. | Springer Verlag | 2025



    Decoupling control of a hypersonic gliding vehicle based on NESO

    Bai, Chen / Ren, Zhang / Shao, Xingyue | IEEE | 2014


    A practical attitude control scheme for hypersonic vehicle based on disturbance observer

    Piao, Minnan / Yang, Zhihong / Sun, Mingwei et al. | SAGE Publications | 2019


    Gliding reentry vehicle lateral/directional coupling attitude control strategy

    Shi, Linan / Li, Huifeng / Zhang, Ran | British Library Online Contents | 2016