Various embodiments of the present invention include assemblies and methods for minimizing the amplitude of attitude jitter. In one embodiment, a flywheel assembly for reducing the amplitude of attitude jitter is provided. The flywheel assembly includes a first flywheel, a second flywheel, and a third flywheel. The first flywheel, second flywheel, and third flywheel are axially aligned and in operable engagement with one another. Each flywheel is configured to be independently controlled in order to manipulate the phase difference therebetween.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    TRIPLE FLYWHEEL ASSEMBLY WITH ATTITUDE JITTER MINIMIZATION


    Beteiligte:

    Erscheinungsdatum :

    2016-05-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F16F SPRINGS , Federn



    TRIPLE FLYWHEEL ASSEMBLY WITH ATTITUDE JITTER MINIMIZATION

    FITZ-COY NORMAN G / NAGABHUSHAN VIVEK | Europäisches Patentamt | 2015

    Freier Zugriff

    Triple flywheel assembly with attitude jitter minimization

    FITZ-COY NORMAN G / NAGABHUSHAN VIVEK | Europäisches Patentamt | 2018

    Freier Zugriff


    Split Flywheel Design with Attitude Jitter Minimization Through Flywheel Phase Control

    Nagabhushan, V. / Fitz-Coy, N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009


    Natural electromagnetic suspension attitude control flywheel motor

    KONG XIANG / LI TIECAI / LING YAN | Europäisches Patentamt | 2023

    Freier Zugriff