The interaction between the automatic docking maneuver and the attitude dynamics of the involved spacecraft is analyzed, as far as the docking maneuver behavior is concerned. Three different docking concepts are investigated by dedicated computer dynamics simulation programs. The simulations consider rigid bodies and the presence of a flexible element between the docking port and the main body on one spacecraft; and with the docking port axis on each vehicle aligned with the center of mass and with large arms with respect to it. The need for proper attitude control systems is established; the importance of energy dissipation sources is shown.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Automatic Docking Maneuver and Attitude Control System


    Contributors:
    A. E. Finzi (author) / F. Venditti (author)

    Publication date :

    1986


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Automatic docking manoeuvre and attitude control system

    Finzi, A.E. / Venditti, F. | Tema Archive | 1986


    Fast satellite attitude maneuver and control

    Ye, Dong / Li, You / Xiao, Yan | TIBKAT | 2022


    Mariner 4 maneuver and attitude control

    Bouvier, H. K. / Forney, R. G. / Szirmay, S. Z. | NTRS | 1969


    Mariner 4 maneuver and attitude control.

    Bouvier, H. K. / Forney, R. G. / Szirmay, S. Z. | NTRS | 1965