Some single-axis floated integrating rate gyroscopes are designed with float suspension systems that have sensible radial compliance. When angular velocities are impressed about the output axis of these units, the resulting gyroscopic torque about the input axis causes the float to cock within the gyro housing. This paper presents complete equations of motion for the single-axis floated gyro, taking into account the float-cocking degree of freedom. Previously observed test results are explained analytically. Approximate expressions for the squeeze-film damping constant, not available in the literature, are developed in Appendix B.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    The Float-Cocking Phenomenon in Single-Axis Floated Gyroscopes


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Paulsen, R. E. (Autor:in)

    Kongress:

    NASA Aerospace Vehicle Flight Control Conference ; 1965



    Erscheinungsdatum :

    1965-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Crossbow cocking apparatus

    VERGARA DAVID | Europäisches Patentamt | 2019

    Freier Zugriff

    CROSSBOW COCKING APPARATUS

    VERGARA DAVID | Europäisches Patentamt | 2017

    Freier Zugriff

    FLOATED INERTIAL PLATFOXMS

    BAKER, L. | AIAA | 1965


    Miniature floated inertial platform

    ALEXANDER, N. | AIAA | 1969


    Alstom floated, Greenbrier in Poland

    British Library Online Contents | 1998