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Attitude control system synthesis for the Hoop/Column antenna using the LQG/LTR methodThis paper investigates the application of the linear-quadratic-Gaussian (LQG)/loop transfer recovery (LTR) method to the problem of synthesizing a fine-pointing control system for a large flexible space anenna. The study is based on an antenna, which consists of three rigid-body rotational modes and the first ten elastic modes. A robust compensator design for achieving the required pointing performance in the presence of modeling uncertainties is obtained using the LQG/LTR method. For the Hoop/Column antenna, a satisfactory controller design meeting a desired bandwidth of .1 rad/sec and ensuring stability with unmodelled high frequency modes is obtained using only a collocated pair of 3-axis attitude sensors and torque actuators. This study also indicates that to achieve the desired performance bandwidth of 0.1 rad/sec. and to ensure stability in the presence of higher frequency elastic modes, the design model should include at least the first three flexible modes together with the rigid body modes.
Document ID
19860062714
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sundararajan, N.
(NASA Langley Research Center Hampton, VA, United States)
Joshi, S. M.
(NASA Langley Research Center Hampton, VA, United States)
Armstrong, E. S.
(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 86-2139
Accession Number
86A47452
Distribution Limits
Public
Copyright
Other

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