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