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