In this chapter, we illustrate the applicability of ET-ADRC in attitude tracking for spacecraft systems. Since the kinematic and dynamic equations of rigid spacecraft possess highly coupled nonlinear characteristics and attitude dynamics may suffer from external disturbances, inertia-matrix uncertainties, and even actuator failures, control systems play an important role in achieving attitude maneuvering, attitude tracking, and high-precision pointing of spacecraft, and the attitude-control problem has attracted significant attention over the past few decades [1–5].


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    Title :

    Event-Triggered Attitude Tracking for Rigid Spacecraft


    Additional title:

    Studies in Systems, Decision and Control


    Contributors:
    Shi, Dawei (author) / Huang, Yuan (author) / Wang, Junzheng (author) / Shi, Ling (author)


    Publication date :

    2021-03-16


    Size :

    22 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English