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.
Automatic Docking Maneuver and Attitude Control System
1986
6 pages
Report
Keine Angabe
Englisch
Automatic docking manoeuvre and attitude control system
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