DocumentCode :
3494175
Title :
A model-based thruster leakage monitor for the Cassini spacecraft
Author :
Lee, Allan Y. ; Brown, M. Jay
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume :
2
fYear :
1998
fDate :
21-26 Jun 1998
Firstpage :
902
Abstract :
The Cassini spacecraft uses thrusters to maintain three-axis attitude control and to perform many other functions. If one of the thrusters leaks, the opposing thrusters will be fired excessively to maintain the commanded attitude. Obviously, the draining of hydrazine and the excessive firings of thrusters must be stopped quickly. A set of three model-based leakage detection monitors has been designed and implemented in the flight software to protect Cassini against the occurrence of this unlikely event. Test results indicate that this design can detect thruster leakage quickly and robustly. Once the leak is detected, the on-board fault protection logic will activate remedial actions which include the swapping of thruster branches
Keywords :
aerospace propulsion; attitude control; computerised monitoring; fault diagnosis; space vehicles; Cassini spacecraft; fault protection; flight software; model-based leakage detection; monitoring; three-axis attitude control; thrusters; Event detection; Fault detection; Leak detection; Logic; Monitoring; Propellants; Protection; Robustness; 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.1998.703537
Filename :
703537
Link To Document :
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