Title :
Case studies for prognostics-enhanced Automated Contingency Management for aircraft systems
Author :
Tang, Liang ; Kacprzynski, Gregory J. ; Goebel, Kai ; Vachtsevanos, George
Author_Institution :
Impact Technol., LLC, Rochester, NY, USA
Abstract :
This paper presents several case studies for using prognostic information in the design of fault tolerant control solutions for flight critical aircraft systems. A hierarchical Automated Contingency Management (ACM) architecture that allows fault accommodation and mitigation at various levels in the system ranging from component level control reconfiguration, system level control reconfiguration, to high level mission re-planning is introduced and illustrated with three case studies, one for each level. Incorporating prognostics in ACM system allows not only fault accommodation, but also failure mitigation via proper control actions based on short term prognosis, and moreover, the establishment of a long term operational plan that optimizes the utility of the entire system based on long term prognostics. The proactive ACM concept and architecture presented in this paper are applicable to many advanced autonomous systems such as deep space probes, unmanned autonomous vehicles, satellites, military and commercial aircrafts.
Keywords :
aircraft control; aircraft maintenance; failure analysis; fault tolerance; planning; ACM system; component level control reconfiguration; failure mitigation; fault accommodation; fault mitigation; fault tolerant control; flight critical aircraft system; hierarchical automated contingency management architecture; high level mission replanning; prognostic information; prognostics-enhanced automated contingency management; system level control reconfiguration; Aerospace control; Automatic control; Contingency management; Control systems; Fault tolerant systems; Level control; Military aircraft; Probes; Remotely operated vehicles; Space vehicles;
Conference_Titel :
Aerospace Conference, 2010 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4244-3887-7
Electronic_ISBN :
1095-323X
DOI :
10.1109/AERO.2010.5446844