For the problem of spatial reorientation of spacecraft from the initial position to terminal one we determine preset trajectory and control, realizing it. Optimization of the preset trajectory according to the given criterion is done. Result of numerical modeling is stated. The suggested algorithms are realized in the control system of the "Egyptsat-1" spacecraft, designed by State Design Office "Yuzhnoe" within framework of the international contract between Ukraine and Egypt.


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    Title :

    Spacecraft angular reorientation control by means of flywheels


    Contributors:

    Published in:

    Publication date :

    2008


    Size :

    9 Seiten, 4 Quellen




    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English