LEOP (Launch and Early Operations Phase) support for two three axis stabilized spacecraft which use very different attitude control systems is addressed. Olympus was launched in Jul. 1989 and Italsat in Jan. 1991. The Olympus and Italsat onboard attitude and orbit control systems are outlined with emphasis on the transfer orbit phase. The ground control systems for both spacecraft are described with a review of the actual operational experience. The different role of the ground control systems are detailed, and the advantages and disadvantages of both systems analyzed. Future trends in the design of the ground control systems are discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Three-Axis Stabilisation in LEOP: Autonomy or Ground Control


    Beteiligte:

    Erscheinungsdatum :

    1991


    Format / Umfang :

    7 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    CBERS-2 LEOP Orbit Analysis

    Orlando, V. / Kuga, H. K. / Tominaga, J. et al. | British Library Conference Proceedings | 2004



    LEOP Simulation Service of a Satellite Simulator for Ground Control System Support

    Cho, Sungki / Lee, Sanguk / Kim, Jae Hoon | AIAA | 2004


    Ground Stations Network Operations for GALILEO LEOP with 4 Satellites

    Faure-Marfany, Fabienne / Nayrac, Fabrice | AIAA | 2018


    Sentinel 2B LEOP Flight Dynamics Operational experience

    Affaitati, Francesco / Sánchez, Javier | AIAA | 2017