When the spacecraft has a low spin rate and precise pointing requirements, the wobble angle must be damped in a time period equivalent to a very few wobble cycles. The design, analysis, and test of a passive pendulum wobble damper are described.
A passive pendulum wobble damper for a low spin rate Jupiter flyby spacecraft
1972-06-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Analysis of pendulum damper for satellite wobble damping
AIAA | 1965
|Analysis of pendulum damper for satellite wobble damping
AIAA | 1964
|Mr. Mills Reports on Jupiter Flyby
NTIS | 1994
The Cassini/Huygens Flyby of Jupiter
NTRS | 2000
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