DocumentCode
3516449
Title
Electronic Prognostics System Implementation on Power Actuator Components
Author
Vohnout, Sonia ; Kozak, Mladen ; Goodman, Douglas ; Harris, Ken ; Judkins, Justin
Author_Institution
Ridgetop Group, Tucson, AZ
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
11
Abstract
Prognostics-enablement of power actuator components involves acquisition and processing of multiple data and sensor inputs. Data collection and fusion creates an accurate prognostic prediction. To that end, Ridgetop has developed an extensible Prognostic Analysis System Platform and a companion Prognostics Telemetry Harness. With an electro-mechanical actuator (EMA) as the focus, this paper describes the extensible architecture for a prognostics health management (PHM) system providing state of health (SoH) and remaining useful life´ (RUL) metrics. The key enabler is the ridgetop prognostics telemetry harness (RPTH), which collects and preprocesses signals relating to the health of dynamically executing components and subsystems. With an ultimate target of 100% up-time, prognostics is an effective tool for managing the corrective early actions required to avoid costly down-time events. An example is detailed using a common EMA and further analysis explores the return-on-investment justifying prognostics adoption.
Keywords
aerospace control; aerospace instrumentation; aerospace testing; electric actuators; maintenance engineering; telemetry; data collection; data fusion; electro-mechanical actuator; electronic prognostics system; power actuator components; prognostics health management; prognostics-enablement; remaining useful life metrics; ridgetop prognostics telemetry harness; state of health metric; Aerospace control; Circuit faults; Circuit testing; Data mining; Hydraulic actuators; Military aircraft; Mission critical systems; Space vehicles; Telemetry; Wireless sensor networks;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526607
Filename
4526607
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