DocumentCode
3584388
Title
PROMIS - A generic PHM methodology applied to aircraft subsystems
Author
Smeulers, J.P.M. ; Zeelen, R. ; Bos, A.
Author_Institution
TPD, TNO, Delft, Netherlands
Volume
6
fYear
2002
fDate
6/24/1905 12:00:00 AM
Firstpage
457802
Abstract
This paper describes the basic concepts of the PROMIS methodology for system´s Prognostic Health Management (PHM). The key elements of the PROMIS methodology are: (i) system health is monitored by continuously measuring so-called Condition Parameters (CPs), representing the physical condition of critical system components, (ii) CPs are derived using model-based estimation processes so that the existing set of sensors is exploited as much as possible, and (iii) the remaining lifetime of components is calculated using aging models and the expected system load.
Keywords
ageing; aircraft testing; condition monitoring; PROMIS; aging model; aircraft subsystem; component lifetime; condition parameters; prognostic health management; system health monitoring; Aging; Aircraft; Condition monitoring; Costs; Filters; Life testing; Logistics; Prognostics and health management; Sensor systems; System testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference Proceedings, 2002. IEEE
Print_ISBN
0-7803-7231-X
Type
conf
DOI
10.1109/AERO.2002.1036156
Filename
1036156
Link To Document