Tethered multiple spacecraft configurations are discussed relative to low Earth orbit, geosynchronous Earth orbit, and one, two, or three dimensional configurations. Attitude control, pointing, and stabilization of such tethered systems are addressed.
Summary presentation of the Constellations Panel
1985-03-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Report of the Constellations Panel
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