The report derives the dynamical model of Engineering Test Satellite-VI (ETS-VI), which is a large-scale high-performance test satellite launched by H-II rocket in the summer launch window of 1994. The mission of ETS-VI is to establish the bus technology necessary for realizing a 2-ton-class geosynchronous three-axis stabilized application satellite. The National Aerospace Laboratory is participating in the on-orbit flight experiments of ETS-VI for the system identification and attitude control. Numerical simulation software have been developed and used to check the onboard control algorithm before launch. The paper describes their details.


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    Title :

    Dynamical Model and Numerical Simulations for Engineering Test Satellite-VI


    Contributors:
    I. Yamaguchi (author) / T. Kida (author)

    Publication date :

    1994


    Size :

    22 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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