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Computer optimization techniques for NASA Langley's CSI evolutionary model's real-time control systemThe evolution and optimization of a real-time digital control system is presented. The control system is part of a testbed used to perform focused technology research on the interactions of spacecraft platform and instrument controllers with the flexible-body dynamics of the platform and platform appendages. The control system consists of Computer Automated Measurement and Control (CAMAC) standard data acquisition equipment interfaced to a workstation computer. The goal of this work is to optimize the control system's performance to support controls research using controllers with up to 50 states and frame rates above 200 Hz. The original system could support a 16-state controller operating at a rate of 150 Hz. By using simple yet effective software improvements, Input/Output (I/O) latencies and contention problems are reduced or eliminated in the control system. The final configuration can support a 16-state controller operating at 475 Hz. Effectively the control system's performance was increased by a factor of 3.
Document ID
19920010422
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Elliott, Kenny B.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Ugoletti, Roberto
(NASA Langley Research Center Hampton, VA, United States)
Sulla, Jeff
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-104223
NAS 1.15:104223
Report Number: NASA-TM-104223
Report Number: NAS 1.15:104223
Meeting Information
Meeting: International Instrumentation Symposium, Instrument Society of America
Location: Las Vegas, NV
Country: United States
Start Date: April 26, 1992
End Date: April 30, 1992
Accession Number
92N19664
Funding Number(s)
PROJECT: RTOP 590-14-61-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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