New algorithm calculates attitude with accuracy to spare. Report describes algorithm for use in determining attitude of spacecraft from incremental-angle output of strapdown gyroscope and star-scanner measurements. Highlights detail of underlying theories and strategies. Presents results of simulation to demonstrate capability of algorithm, and discusses possible applications.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Determining Spacecraft Attitude For Planetary Mapping


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.03.1988



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Attitude Control of Spacecraft Swarms for Visual Mapping of Planetary Bodies

    Nallapu, Ravi teja / Thangavelautham, Jekanthan | IEEE | 2019


    Inertial attitude determination for a dual-spin planetary spacecraft

    Wong, E. C. / Breckenridge, W. G. | NTRS | 1983


    New methods of determining spacecraft attitude

    Pitts, R. / Jackson, T. / Gilmozzi, R. | NTRS | 1990


    Inertial attitude determination for a dual-spin planetary spacecraft

    WONG, E. C. / BRECKENRIDGE, W. G. | AIAA | 1983