Part I of this work deals with the use of electrodynamic forces for control of tethered satellite system. A system formed by two massive end-bodies connected to each other by a current carrying tether is to be kept in an Earth-pointing orientation by means of joint actions of thrusters on one of the end-bodies and electrodynamic forces acting on the tether.<>


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Electrodynamic forces in tethered satellite systems. I. System control


    Contributors:
    Netzer, E. (author) / Kane, T.R. (author)


    Publication date :

    1994-10-01


    Size :

    610995 byte




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English