DocumentCode
2791161
Title
Fault Protection for the Space Interferometry Mission
Author
Peer, Scott
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA
fYear
2005
fDate
5-12 March 2005
Firstpage
1
Lastpage
7
Abstract
The Space Interferometry Mission (SIM) is a deep space mission with limited ground contact and challenging instrument fault protection requirements. Some faults that could occur on SIM have symptoms only visible in the scientific measurements, and many of the observations that SIM makes must be repeated to be useful. Because of this, SIM needs to be very reliable. We are addressing these challenges by combining several approaches. The use of redundancy in the instrument will be important in making the complex instrument with several dozen actuators reliable. Probabilistic risk assessment and reliability modeling are being performed to study the most cost effective areas for redundancy. Ground checks are important parts of the fault detection approach. Special approaches such as "flood mode" (providing large amounts of raw data) and diagnostic data dumps are also important
Keywords
aerospace safety; fault location; redundancy; reliability; risk management; Space Interferometry Mission; complex instrument; deep space mission; diagnostic data dump; fault detection; fault protection requirements; flood mode; ground checks; instrument redundancy; probabilistic risk assessment; reliability modeling; scientific measurements; Actuators; Costs; Fault detection; Floods; Instruments; Interferometry; Protection; Redundancy; Risk management; Space missions;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2005 IEEE
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-8870-4
Type
conf
DOI
10.1109/AERO.2005.1559526
Filename
1559526
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