Eddy current nutation damper with progressive damping factor

Aeronautics and astronautics – Spacecraft – Attitude control

Patent

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Details

188 1B, 244166, 310105, B64G 110

Patent

active

041680480

ABSTRACT:
A nutation damper apparatus capable of damping small nutation angles in a satellite. A permanent magnet mounted on the free end of a pendulum arm oscillates back and forth parallel to an adjacent conductive plate in the form of a circular segment having a cross-sectional area that increases from the center to its lateral ends, and induces in the plate a magnetic flux which is proportional to the deviation angle of the pendulum from its rest position.

REFERENCES:
patent: 3510705 (1970-05-01), O'Neill et al.
patent: 3806062 (1974-04-01), Hofmann et al.

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