Flywheels can serve not only as attitude control devices, but also as energy storage devices, thereby eliminating the need for conventional batteries. Hence, a combined energy and attitude control system (CEACS) consisting of a double counter rotating flywheel assembly is proposed for small satellites in this paper. The energy level in CEACS depends mainly on the flywheels' speeds. Therefore, a specific flywheel energy management strategy has to be implemented to take into account the limitations of the flywheels, which has not been established until today.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Flywheel energy storage for spacecraft


    Contributors:

    Published in:

    Publication date :

    2004-08-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Flywheel energy storage for spacecraft

    Gross, S. | Tema Archive | 1984


    Flywheel energy storage for spacecraft

    Varatharajoo, Renuganth | Online Contents | 2004


    Flywheel Energy Storage for Spacecraft Power Systems

    Patel, Mukund R. | SAE Technical Papers | 1999



    MAGNETIC UNLOADING OF SPACECRAFT FLYWHEEL ENGINES

    GALKIN DMITRIJ IGOREVICH / SIMON JANTS ROSTISLAV PETROVICH | European Patent Office | 2015

    Free access