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Spacecraft Attitude Control Using A Smart Control SystemTraditionally, spacecraft attitude control has been implemented using control loops written in native code for a space hardened processor. The Naval Research Lab has taken this approach during the development of the Attitude Control Electronics (ACE) package. After the system was developed and delivered, NRL decided to explore alternate technologies to accomplish this same task more efficiently. The approach taken by NRL was to implement the ACE control loops using systems technologies. The purpose of this effort was to: (1) research capabilities required of an expert system in processing a classic closed-loop control algorithm; (2) research the development environment required to design and test an embedded expert systems environment; (3) research the complexity of design and development of expert systems versus a conventional approach; and (4) test the resulting systems against the flight acceptance test software for both response and accuracy. Two expert systems were selected to implement the control loops. Criteria used for the selection of the expert systems included that they had to run in both embedded systems and ground based environments. Using two different expert systems allowed a comparison of the real-time capabilities, inferencing capabilities, and the ground-based development environment. The two expert systems chosen for the evaluation were Spacecraft Command Language (SCL), and NEXTPERT Object. SCL is a smart control system produced for the NRL by Interface and Control Systems (ICS). SCL was developed to be used for real-time command, control, and monitoring of a new generation of spacecraft. NEXPERT Object is a commercially available product developed by Neuron Data. Results of the effort were evaluated using the ACE test bed. The ACE test bed had been developed and used to test the original flight hardware and software using simulators and flight-like interfaces. The test bed was used for testing the expert systems in a 'near-flight' environment. The technical approach, the system architecture, the development environments, knowledge base development, and results of this effort are detailed.
Document ID
19930002744
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Brian Buckley
(Interface and Control Systems West Melbourne, FL, United States)
Louis Wheatcraft
(Barrios Technology, Inc. Houston, TX., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Publication Information
Publication: Fifth Annual Workshop on Space Operations Applications and Research (SOAR 1991)
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
NASA/CP-3127/Vol I
Meeting Information
Meeting: Space Operation, Application and Research Symposium
Location: Houston, TX
Country: US
Start Date: July 9, 1991
End Date: July 11, 1991
Sponsors: National Aeronautics and Space Administration, U.S. Air Force Phillips Laboratory, University of Houston - Clear Lake
Accession Number
93N11932
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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