NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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
19930053877
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Elliott, Kenny B.
(NASA Langley Research Center 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
August 16, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: International Instrumentation Symposium, 38th, Las Vegas, NV, Apr. 26-30, 1992, Proceedings (A93-37851 15-35)
Publisher: Instrument Society of America
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
93A37874
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available