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