DocumentCode :
326835
Title :
A state-space fault monitor architecture and its application to the Cassini spacecraft
Author :
Macale, G.A.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
Volume :
2
fYear :
1998
fDate :
21-26 Jun 1998
Firstpage :
899
Abstract :
The Cassini spacecraft fault protection design includes fault monitors that use a state-space architecture to monitor the performance of spacecraft functions. This paper reports on the design of these monitors
Keywords :
computerised monitoring; fault diagnosis; space telemetry; space vehicles; state-space methods; Cassini spacecraft; fault monitoring; fault protection design; state-space architecture; telemetry; Attitude control; Digital filters; Equations; Information filtering; Information filters; Monitoring; Position measurement; Protection; Space vehicles; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1998. Proceedings of the 1998
Conference_Location :
Philadelphia, PA
ISSN :
0743-1619
Print_ISBN :
0-7803-4530-4
Type :
conf
DOI :
10.1109/ACC.1998.703536
Filename :
703536
Link To Document :
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