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Vibrationally Excited Satellite Attitude Actuator: a Feasibility Study
Date
2015-06-19
Author
Akbulut, Burak
Tekinalp, Ozan
Azgın, Kıvanç
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A new attitude control actuator, the vibrating mass gyroscope is considered. The actuator transforms the vibratory motion of a single gimbal gyroscope to a positive or negative, fluctuating control torque. The equations of motion for such an actuator are presented. The feasibility of construction of such an actuator is investigated. Possible means of realizing the vibratory motion is proposed.
Subject Keywords
Attitude actuator
,
Satellite
,
Dynamics
,
Torque amplification
URI
https://hdl.handle.net/11511/53850
Collections
Department of Aerospace Engineering, Conference / Seminar
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B. Akbulut, O. Tekinalp, and K. Azgın, “Vibrationally Excited Satellite Attitude Actuator: a Feasibility Study,” 2015, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/53850.