Abstract In this paper, feedback attitude control of an underactuated spacecraft with two single gimbal control moment gyros (SGCMGs) is considered. For a two-SGCMG system in an arbitrary configuration, a feedback control method based on a real-time optimization approach is proposed. Here, the gimbal angle trajectories as the solution to the minimum-time control are parameterized by the time polynomials, and their coefficients are modified at each sampling period. Numerical simulations are performed to demonstrate the validity of the proposed method as well as a certain robustness against unmodeled dynamics. Furthermore, the experimental verification is also conducted to demonstrate the actual effectiveness.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Feedback attitude control of spacecraft using two single gimbal control moment gyros


    Contributors:

    Published in:

    Advances in Space Research ; 68 , 7 ; 2713-2726


    Publication date :

    2021-05-11


    Size :

    14 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Spacecraft Attitude Maneuver using Two Single-gimbal Control Moment Gyros

    Kasai, Shinya / Kojima, Hirohisa / Satoh, Mitsunori | AIAA | 2012


    Spacecraft Attitude Maneuver using Two Single-gimbal Control Moment Gyros

    Kasai, S. / Kojima, H. / Satoh, M. et al. | British Library Conference Proceedings | 2012



    Spacecraft attitude maneuver using two single-gimbal control moment gyros

    Kasai, Shinya / Kojima, Hirohisa / Satoh, Mitsunori | Elsevier | 2012


    Two Parallel Single-Gimbal Control Moment Gyros Actuated Spacecraft Attitude Maneuver

    Yue, Chengfei / Wu, Fan / Wang, Feng et al. | IEEE | 2020