According to attitude control of a hypersonic gliding vehicle, a decoupling control approach based on NESO is proposed. Decoupling control is realized through the decentralized control theory. The system coupling terms and uncertainties are estimated by NESO and added into the control law for compensation. Theoretical analysis proves that the tracking errors of the closed-loop system are consistently bounded. Simulations are carried on through the hypersonic gliding vehicle model comparing the proposed method and the traditional sub-channel control method. The results show that the tracking effectiveness of the proposed method is better and impact caused by coupling and uncertainties is eliminated.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Decoupling control of a hypersonic gliding vehicle based on NESO


    Contributors:
    Bai, Chen (author) / Ren, Zhang (author) / Shao, Xingyue (author)


    Publication date :

    2014-07-01


    Size :

    232592 byte





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Hypersonic Cruise Vehicle Attitude Control Based on NESO

    Lian, Cheng-Bin / Bai, Chen / Ren, Zhang et al. | Tema Archive | 2013


    Hypersonic Cruise Vehicle Attitude Control Based on NESO

    Lian, Cheng Bin ;Bai, Chen ;Ren, Zhang | Trans Tech Publications | 2013


    Observer-based attitude control for hypersonic gliding vehicle

    Gao, Kehan / Li, Qingdong / Ren, Zhang et al. | IEEE | 2014


    Fault-tolerant reconfigurable control for reusable launch vehicle using NESO

    Shao, Xingyue / Li, Qingdong / Ren, Zhang et al. | IEEE | 2014


    Observer Based Fixed-Time Tracking Control for Hypersonic Gliding Vehicle

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