An adaptive control scheme for the attitude control of a rigid spacecraft is derived using a linear parameterization of the equation of motion. The tracking error is described with the Euler parameter vector. Global convergence of the tracking error to zero is shown using passivity theory. This allows for the use of time-varying positive-definite feedback gain matrices, and the results can easily be extended to other passive parameter update laws.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Passivity-based adaptive attitude control of a rigid spacecraft


    Additional title:

    Passivitätsbasierte adaptive Fluglagenregelung eines starren Raumfahrzeugs


    Contributors:
    Egeland, O. (author) / Godhavn, J.M. (author)

    Published in:

    Publication date :

    1994


    Size :

    5 Seiten, 2 Bilder, 16 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Spacecraft attitude passivity control based on PCH model

    Wang, Qing / Gong, Ligang / Dong, Chaoyang | British Library Online Contents | 2017


    Passivity-Based Pulse-Width-Modulated Spacecraft Attitude Control

    Lang, Xiaoyu / de Ruiter, Anton | AIAA | 2021


    Improved Adaptive Sliding Mode Control for Rigid Spacecraft Attitude Tracking

    Cong, Binglong / Chen, Zhen / Liu, Xiangdong | ASCE | 2012



    Finite-time adaptive fault-tolerant attitude control for rigid spacecraft

    Geng, Yunhai / Hu, Jian / Bai, Yuliang et al. | IEEE | 2018