Aeronautics and astronautics – Spacecraft – Attitude control
Patent
1993-03-12
1994-08-02
Barefoot, Galen L.
Aeronautics and astronautics
Spacecraft
Attitude control
188378, 248550, 364508, B64G 138
Patent
active
053338197
ABSTRACT:
A vibration suppression system senses undesired mechanical motion of a body, and continuously drives a proof mass actuator system to reduce disturbances. An inertial or relative displacement sensor is processed to determine the energy content of the motion, and a correction signal is generated which is summed with the actuator drive signal to minimize the sensed motion energy. The position of the proof mass is sensed, and processed by differentiating and scaling, and the processed proof mass position signal is also summed with the actuator drive signal. The system causes the proof mass actuator loop natural frequency to tend to track the frequency associated with the maximum vibrational energy.
REFERENCES:
patent: 3836098 (1974-09-01), Miyashita
patent: 4083433 (1978-04-01), Geohegan, Jr. et al.
patent: 4470121 (1984-09-01), Eberf
patent: 4483425 (1984-11-01), Newman
patent: 4922159 (1990-05-01), Phillips et al.
patent: 5131611 (1992-07-01), Vollaro
patent: 5209326 (1993-05-01), Harper
Barefoot Galen L.
Berard C. A.
General Electric Company
Meise W. H.
Young S. A.
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