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modeling and tachometer feedback in the control of an experimental single link flexible structureIn this work a formulation for the modeling of a single link flexible structure will be introduced that includes the effects of dynamic interaction between the actuator and structure. These effects are the rotational modal participation factors for the structure's vibratory motion that occurs at the slewing axis. It will be shown, both theoretically and experimentally, that this dynamic interaction can be advantageous for vibration suppression of the flexible modes of the system during slewing positioning maneuvers.
Document ID
19910050917
Document Type
Conference Paper
Authors
Garcia, Ephrahim
(State Univ. of New York Buffalo, NY, United States)
Inman, Daniel J.
(New York, State University Buffalo, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Meeting Information
International Modal Analysis Conference(Kissimmee, FL)
Funding Number(s)
CONTRACT_GRANT: F49620-86-C-0011
CONTRACT_GRANT: NGT-33-183-804
Distribution Limits
Public
Copyright
Other