DocumentCode
2818916
Title
Experimental study of active vibration suppression of flexible structure using modular control patch
Author
Song, Gangbing ; Schmidt, Steve P. ; Agrawal, Brij N.
Author_Institution
Spacecraft Res. & Design Centre, US Naval Postgraduate Sch., Monterey, CA, USA
Volume
1
fYear
1998
fDate
21-28 Mar 1998
Firstpage
189
Abstract
This paper presents experimental results of vibration suppression of a flexible structure using a miniaturized digital controller, called modular control patch (MCP). The MCP employs a TI-C30 digital signal processor and was developed by TRW for the United States Air Force for future space vibration control. In this research, the MCP is used to implement different control algorithms for vibration suppression of a cantilevered aluminum beam with piezoceramic sensors and actuators. Positive position feedback (PPF) control, strain rate feedback (SRF) control, and their combinations were implemented. Experiments found that PPF control is most effective for single-mode vibration suppression, and two PPF filters in parallel are most effective for multi-mode vibration suppression. Further experiments demonstrated the robustness of PPF control. PPF can achieve effective vibration suppression when there is a 20% error in modal frequency
Keywords
aerospace control; digital control; feedback; flexible structures; robust control; vibration control; TI-C30 digital signal processor; active vibration suppression; cantilevered beam; flexible structure; miniaturized digital controller; modal frequency; modular control patch; piezoceramic sensors; positive position feedback; robustness; space vibration control; strain rate feedback; Aluminum; Digital control; Digital signal processors; Feedback; Flexible structures; Force sensors; Signal processing algorithms; Strain control; Structural beams; Vibration control;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 1998 IEEE
Conference_Location
Snowmass at Aspen, CO
ISSN
1095-323X
Print_ISBN
0-7803-4311-5
Type
conf
DOI
10.1109/AERO.1998.686818
Filename
686818
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