DocumentCode :
296860
Title :
System fault protection design for the Cassini spacecraft
Author :
Slonski, John P.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume :
1
fYear :
1996
fDate :
3-10 Feb 1996
Firstpage :
279
Abstract :
Fault protection can include a wide range of topics, ranging from fault prevention to autonomous fault detection and recovery. This paper will address a portion of the autonomous fault detection and recovery implemented on board the Cassini spacecraft. Specifically, the topic is system level fault protection design, as opposed to subsystem fault protection design. The design of system fault protection for the Cassini spacecraft will be described at a high level in order to define the guiding principles of the design. This will include examining driving requirements, high level design trades, and major architectural elements, including practical details of their design. Finally, a detailed design description will be given of two Cassini fault protection responses which are likely to be used on most other spacecraft
Keywords :
aerospace computing; aerospace control; command and control systems; protection; reliability; special purpose computers; system recovery; Cassini spacecraft; Saturn system exploration; architectural elements; autonomous fault detection and recovery; command and data subsystem; command loss; concurrent faults; driving requirements; fault recovery responsibility allocation; high level design trades; onboard fault detection; prioritisation; spacecraft safing; system fault protection design; system level design; Aerospace electronics; Fault detection; Instruments; NASA; Plasma waves; Probes; Propulsion; Protection; Radioactive materials; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Applications Conference, 1996. Proceedings., 1996 IEEE
Conference_Location :
Aspen, CO
Print_ISBN :
0-7803-3196-6
Type :
conf
DOI :
10.1109/AERO.1996.495890
Filename :
495890
Link To Document :
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