Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Attitude Stability of a Spinning Spacecraft During Appendage Deployment/Retraction



    Kongress:

    Symposium, Flight mechanics/estimation theory ; 1994 ; Greenbelt; MD



    Erscheinungsdatum :

    1994-01-01


    Format / Umfang :

    4 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Appendage Deployment Verification for the 2001 Mars Odyssey Spacecraft Using Spacecraft Attitude Telemetry (AAS 03-075)

    Gehling, R. / Linch, S. / American Astronautical Society | British Library Conference Proceedings | 2003


    The Attitude Control of Small Spacecraft with Movable Appendage

    Han, C. / Guo, J. / You, Z. et al. | British Library Conference Proceedings | 2003


    The Attitude Control of Small Spacecraft with Movable Appendage

    Han, Congying / Guo, Jian / You, Zheng et al. | AIAA | 2003


    Deployment and Retraction Mechanisms for Spinning Solar Sail Membrane

    Furuya, Hiroshi / Satou, Yasutaka | AIAA | 2008