DocumentCode :
1769766
Title :
Spacecraft health monitoring and management systems
Author :
Tipaldi, Massimo ; Bruenjes, Bernhard
Author_Institution :
Compagnia Gen. per lo Spazio, Benevento, Italy
fYear :
2014
fDate :
29-30 May 2014
Firstpage :
68
Lastpage :
72
Abstract :
Spacecraft health monitoring and management systems (also referred to as FDIR (Fault Detection, Isolation and Recovery) systems)) are addressed since the very beginning of any space mission design and play a relevant role in the definition of their reliability, availability and safety objectives. Their primary purposes are the safety of spacecraft/mission life and the improvement of its service availability. In this paper current technical and programmatic FDIR strategies are presented along with their strong connection with the wider concept of on-board autonomy, which is becoming the key-point in the design of new-generation spacecrafts. Recent projects developed at OHB System AG have brought to light some issues in the current FDIR system design approaches. These findings pave the way for innovative solutions, which can support and not rule out conventional industrial practices.
Keywords :
aerospace safety; condition monitoring; fault diagnosis; space vehicles; AG; OHB System; fault detection isolation and recovery system; on-board autonomy; programmatic FDIR strategies; space mission design; spacecraft health management system; spacecraft health monitoring system; spacecraft-mission life safety; Hardware; Mathematical model; Monitoring; Redundancy; Satellites; Software; Space vehicles; FDIR; Packet Utilization Standard; Spacecraft Autonomy; Spacecraft Health Monitoring;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Metrology for Aerospace (MetroAeroSpace), 2014 IEEE
Conference_Location :
Benevento
Type :
conf
DOI :
10.1109/MetroAeroSpace.2014.6865896
Filename :
6865896
Link To Document :
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