This paper presents design, implementation and experimental results of active vibration control of Naval Postgraduate School (NPS) space truss using a piezoelectric ceramic stack actuator. The NPS space truss represents a flexible spacecraft structure that may support interferometer, antenna and other vibration-sensitive instrumentation. To simulate the effects of a spacecraft disturbance on the truss, a proof mass actuator is incorporated on the structure to excite the truss. To reduce the vibrations caused by the proof mass actuator, an active strut member is installed along a diagonal of the base bay of the truss. The active strut element consists of a piezoelectric ceramic actuator stack, a force transducer and mechanical interfaces. An integral plus double-integral force controller is designed to suppress vibration of the truss. Experimental results demonstrate that the active piezoceramic strut actuator can effectively reduce truss vibration.
Active vibration control of a space truss using a lead zirconate titanate stack actuator
2001
7 Seiten, 14 Quellen
Article (Journal)
English
Active vibration control of a space truss using a lead zirconate titanate stack actuator
Online Contents | 2001
|Active vibration control of a space truss using a lead zirconate titanate stack actuator
SAGE Publications | 2001
|SAE Technical Papers | 2000
|British Library Conference Proceedings | 2000
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