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Reuse and Interoperability of Avionics for Space SystemsThe space environment presents unique challenges for avionics. Launch survivability, thermal management, radiation protection, and other factors are important for successful space designs. Many existing avionics designs use custom hardware and software to meet the requirements of space systems. Although some space vendors have moved more towards a standard product line approach to avionics, the space industry still lacks similar standards and common practices for avionics development. This lack of commonality manifests itself in limited reuse and a lack of interoperability. To address NASA s need for interoperable avionics that facilitate reuse, several hardware and software approaches are discussed. Experiences with existing space boards and the application of terrestrial standards is outlined. Enhancements and extensions to these standards are considered. A modular stack-based approach to space avionics is presented. Software and reconfigurable logic cores are considered for extending interoperability and reuse. Finally, some of the issues associated with the design of reusable interoperable avionics are discussed.
Document ID
20070022268
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hodson, Robert F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2007
Subject Category
Avionics And Aircraft Instrumentation
Report/Patent Number
AIAA 207-2918
Report Number: AIAA 207-2918
Meeting Information
Meeting: Infotech@Aerospace 2007 Conference and Exhibit
Location: Rohnert Park, CA
Country: United States
Start Date: May 7, 2007
End Date: May 10, 2007
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 60476.02.06.08.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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