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
Conference paper
No indication
English
Analysis of pendulum damper for satellite wobble damping
AIAA | 1965
|Analysis of pendulum damper for satellite wobble damping
Engineering Index Backfile | 1965
|Analysis of pendulum damper for satellite wobble damping
AIAA | 1964
|Mr. Mills Reports on Jupiter Flyby
NTIS | 1994