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Fault protection techniques in JPL SpacecraftWhile every JPL spacecraft requires some unique mission specific fault protection, there are many requirements which are common to all spacecraft configurations. These consist of protecting command and data processing & attitude control computers, protection against communication loss with the spacecraft, ensuring that safe external and internal temperature levels are maintained, and recovery from power overloads. Additionally, most JPL spacecraft are equipped with a general-purpose 'Safe Mode' response algorithm which configures the spacecraft to a lower power state which is safe and predictable so that diagnosis of more complex faults can be addressed by the Operations Team. This paper details the generic application of fault protection techniques which are implemented into most JPL spacecraft designs.
Document ID
20060044316
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Morgan, Paula S.
Date Acquired
August 23, 2013
Publication Date
November 7, 2005
Meeting Information
Meeting: First International Forum on Integrated System Health Engineering and Management in Aerospace (ISHEM)
Location: NAPA, CA
Country: United States
Start Date: November 7, 2005
End Date: November 10, 2005
Distribution Limits
Public
Copyright
Other
Keywords
fault protection

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