In this article, attitude coordination control for flexible spacecraft formation flying is investigated in the condition that common reference attitude is only available to a subset of the followers of the group. Measurement errors, immeasurable flexible modal variables, external disturbances, and model uncertainties of both rigid and flexible dynamics are addressed concurrently. Then, based on the sequential Lyapunov method, successively less conservative attitude coordination performance bounds can be obtained with the proposed distributed attitude coordination controller.


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    Title :

    Attitude Coordination Control for Flexible Spacecraft Formation Flying With Guaranteed Performance Bounds


    Contributors:
    Xiao, Yan (author) / de Ruiter, Anton (author) / Ye, Dong (author) / Sun, Zhaowei (author)


    Publication date :

    2023-04-01


    Size :

    3122821 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English