期刊
出版社
SAGE PUBLICATIONS LTD
DOI: 10.1177/0954406218756941
关键词
Vibration control; Stewart platform; voice coil motor; Newton-Euler method; decentralized control
资金
- Foundation of Civil Astronautics
- Pre-research Foundation of General Armament Department of China
In pursuit of a better working performance of the precise instruments equipped in spacecraft, vibration control systems are essential for preventing them from being disturbed. This paper studies the decentralized vibration control problems of a voice coil motor-based Stewart parallel mechanism. The Newton-Euler Method is used to formulate the dynamical equations of the Stewart platform in joint space. The decentralized control theory is employed to design the controller for the linearized system. A prototype of the voice coil motor-based Stewart platform was designed and tested to validate the vibration attenuation performance of the decentralized system. The effectiveness of active vibration isolation system is revealed by both the simulation and real-time experiments.
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