OPTIMAL ACTIVE VIBRATION ABSORBER - DESIGN AND EXPERIMENTAL RESULTS

被引:15
|
作者
LEEGLAUSER, G
JUANG, JN
SULLA, JL
机构
[1] Department of Mechanical and Aeronauticai Engineering, Clarkson University, Potsdam, NY
[2] Spacecraft Dynamics Branch, NASA Langiey Research Center, Hampton, VA
[3] Lockheed Engineering and Sciences Company, Hampton, VA
关键词
D O I
10.1115/1.2873874
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
An optimal active vibration absorber can provide guaranteed closed-loop stability and control for large flexible space structures with collocated sensors/actuators. The active vibration absorber is a second-order dynamic system which is designed to suppress any unwanted structural vibration. This can be designed with minimum knowledge of the controlled system. Two methods for optimizing the active vibration absorber parameters are illustrated: minimum resonant amplitude and frequency matched active controllers. The Controls-Structures interaction Phase-1 Evolutionary Model at the NASA Langley Research Center is used to demonstrate the effectiveness of the active vibration absorber for vibration suppression. Performance is compared numerically and experimentally using acceleration feedback.
引用
收藏
页码:165 / 171
页数:7
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