Simulation and testing of digital control on a flexible beamLarge space structures are expected to have control problems due to low stiffness and damping, and control laws for these structures must deal with shape and configuration control as well as attitude and orbit maintenance. In general, these control tasks must be accomplished without adversely interacting with the lightly damped and low frequency vibration modes of the structure. Modal control schemes have been proposed to deal with these problems. A discrete time parameter adaptive control scheme which uses modal control has been proposed by Montgomery and Johnson (1978). In the present investigation the method considered by Montgomery and Johnson is applied to a homogeneous free-free beam in both numerical simulation and laboratory experimentation. Mathematical modeling of the beam is treated in a manner expedient for digital simulation and control implementation.
Document ID
19820055433
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Williams, J. P. (NASA Langley Research Center Hampton, VA, United States)
Montgomery, R. C. (NASA Langley Research Center Spacecraft Control Branch, Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 82-1569Report Number: AIAA PAPER 82-1569