The Space Flyer Unit (SFU) is a retrievable and reusable platform which will be utilized for many kinds of scientific and engineering experiments in space. SFU was launched by a Japanese H2 launch vehicle and is to be retrieved by a U.S. Shuttle orbiter. The functions of the navigation, guidance and control subsystem (NGC) of SFU are autonomous navigation and guidance for rendezvous with STS using Global Positioning System (GPS), Inertial Measurement Unit (IMU), and NGC Computer (NGCC), as well as attitude control of an ordinary three axis controlled spacecraft. The design status of autonomous navigation and guidance logic for rendezvous with STS, and ground support functions are discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Navigation and Guidance Technique for SFU's Rendezvous with Space Shuttle


    Beteiligte:
    K. Ninomiya (Autor:in) / T. Nishimura (Autor:in) / T. Yamaguchi (Autor:in) / M. Sato (Autor:in) / K. Tsukahara (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Onboard rendezvous navigation for the Space Shuttle

    Wylie, A. D. / Devezin, H. G. | NTRS | 1985


    Rendezvous guidance with proportional navigation

    Yuan, Pin-Jar / Hsu, Shih-Che | AIAA | 1994


    Rendezvous Guidance with Proportional Navigation

    Yuan, P.-J. | Online Contents | 1994


    Rendezvous Guidance with Proportional Navigation

    Yuan, P. J. / Hsu, S. C. / Yang, C. Y. | British Library Conference Proceedings | 1993