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Positive position feedback control for large space structuresA new technique for vibration suppression in large space structures is investigated in laboratory experiments on a thin cantilever beam. This technique, called Positive Position Feedback, makes use of generalized displacement measurements to accomplish vibration suppression. Several features of Positive Position Feedback make it attractive for the large space structure control environment: The realization of the controller is simple and straightforward. Global stability conditions can be derived which are independent of the dynamical characteristics of the structure being controlled, i.e., all spillover is stabilizing. The method cannot be destabilized by finite actuator dynamics, and the technique is amenable to a strain-based sensing approach. The experiments control the first six bending modes of a cantilever beam, and make use of piezoelectric materials for actuators and sensors, simulating a piezoelectric active-member. The modal damping ratios are increased by factors ranging from 2 to 130.
Document ID
19870046437
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fanson, J. L.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Caughey, T. K.
(California Institute of Technology Pasadena, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 87-0902
Accession Number
87A33711
Distribution Limits
Public
Copyright
Other

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