DocumentCode
1746917
Title
Goal-based fault tolerance for space systems using the mission data system
Author
Rasmussen, Robert D.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
5
fYear
2001
fDate
2001
Firstpage
2401
Abstract
In anticipating insitu exploration and other circumstances with environmental uncertainty, the present model for space system fault tolerance breaks down. The perplexities of fault-tolerant behavior, once confined to infrequent episodes, must now extend to the entire operational model. To address this dilemma we need a unified approach to robust behavior that includes fault tolerance as an intrinsic feature. This requires an approach capable of measuring operators´ intent in the light of present circumstances, so that actions are derived by reasoning, not by edict. The Mission Data System (MDS), presently under development by NASA is one realization of this paradigm -part of a larger effort to provide multi-mission flight and ground software for the next generation of deep space systems. This paper describes the MDS approach to fault tolerance, contrasting it with past efforts, and offering motivation for the approach as a general recipe for similar efforts
Keywords
aerospace computing; aerospace control; fault diagnosis; fault tolerance; reliability; space vehicle electronics; systems engineering; deep space systems; fault tolerance; ground software; mission data system; multi-mission flight software; operational mode; robust behavior; Data systems; Fault tolerance; Fault tolerant systems; Object oriented modeling; Reliability engineering; Robustness; Space missions; Space technology; Space vehicles; Systems engineering and theory;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-6599-2
Type
conf
DOI
10.1109/AERO.2001.931199
Filename
931199
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