The novel discrete algorithms for signal processing, calibration and alignment of a strapdown inertial navigation system for attitude determination of an agile spacecraft are presented. The problem on synthesis of the attitude guidance laws for an observation spacecraft at land surveying is considered. The spacecraft attitude guidance on selected sequence by interchanging its agile rotation maneuvers with the general boundary conditions and the scanning observation courses is performed by a gyro moment cluster. Numerical results demonstrating efficiency of the developed methods for the stellar-inertial navigation and synthesis of the gyromoment guidance laws at the area land survey are presented.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Methods for stellar-inertial navigation and gyromoment guidance of the agile land-survey satellites


    Beteiligte:
    Somov, Y. (Autor:in) / Buryrin, S. (Autor:in) / Somov, S. (Autor:in)


    Erscheinungsdatum :

    01.06.2011


    Format / Umfang :

    1736187 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Attitude guidance, navigation and robust control of an agile land-survey satellite

    Somov, Yevgeny / Butyrin, Sergey / Somov, Sergey | IEEE | 2017


    Stellar Inertial Navigation Workstation

    Johnson, W. / Johnson, B. / Swaminathan, N. | NTRS | 1989


    Reusable Stellar Inertial Attitude Determination (SIAD) Design for Spacecraft Guidance, Navigation & Control

    Li, Rongsheng (Ken) / Needelman, David / Fowell, Richard et al. | AIAA | 2005