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Design of robust line-of-sight pointing control system for the SCOLE configurationRobust compensator design for attitude control of the Spacecraft Control Laboratory Experiment (SCOLE) configuration is considered. A loop-shaping procedure similar to that used in the LQG/LTR method is used to iteratively design the compensator. A satisfactory compensator is obtained by including the rigid modes and three elastic modes in the design model.
Document ID
19880040140
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
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 13, 2013
Publication Date
January 1, 1987
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 1987 American Control Conference
Location: Minneapolis, MN
Country: United States
Start Date: June 10, 1987
End Date: June 12, 1987
Sponsors: American Automatic Control Council
Accession Number
88A27367
Distribution Limits
Public
Copyright
Other

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