Control effectiveness characterization for state estimation and control on a highly flexible gridControl effectiveness tests of reaction wheel actuators on a highly flexible grid are reported herein. Analytic determination of actuator control effectiveness is accomplished with finite element modelling. Experimental determination is done with two algorithms. The first is an equation error parameter identification scheme which estimates the control coefficients of the second order difference equation model of each vibration mode. The second is a least square error algorithm using the same model. For both methods there is a lack of agreement with analytic prediction.
Document ID
19860062716
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Montgomery, R. C. (NASA Langley Research Center Hampton, VA, United States)
Williams, J. P. (NASA Langley Research Center Hampton, VA, United States)
Lazarus, T. L. (NASA Langley Research Center Hampton, VA, United States)
Nelson, P. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 86-2142Report Number: AIAA PAPER 86-2142