Dynamic Decision Support (D2S) for Real-Time Assessment of System Health and Fault Contingency Planning

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$79,854.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
N68335-06-C-0073
Award Id:
75298
Agency Tracking Number:
N052-104-0419
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
200 Canal View Boulevard, Rochester, NY, 14623
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
073955507
Principal Investigator:
MichaelRoemer
Director of Engineering
(585) 424-1990
mike.roemer@impact-tek.com
Business Contact:
MarkRedding
President
(585) 424-1990
mark.redding@impact-tek.com
Research Institute:
n/a
Abstract
Impact Technologies, in collaboration with Honeywell Engines and Systems, propose to develop an innovative Dynamic Decision Support (D2S) concept for critical aircraft systems using simulation-based fault classifiers and adaptive contingency management techniques, which will be implemented through a real-time software agent architecture. The significant technology advancement proposed herein is based on using dynamic model simulations in a real-time computing environment to not only diagnose faults, but also to determine "on the fly" how accommodate for them. Current on-board technologies have to map fault conditions to an associated set of pre-determined contingency plans, which can not possibly account for the entire set of fault scenarios that can occur in flight. Hence, the innovations of this project include: 1) Development and demonstration of an agent-based software architecture that is capable of executing simulation models of critical aircraft systems with an adaptive flight control component that performs fault contingency management in real-time; 2) Develop simulation-based fault classification algorithms for the Honeywell Power Thermal Management System (PTMS) with real-time functionality in all system operating modes; 3) Develop contingency management algorithms using dynamic performance assessment calculations and flight control command generation under faulty aircraft system dynamics constraints; and 4) Develop a Simulink-based demonstration of the dynamic contingency management and fault-adaptive control system with application to the Honeywell PTMS.

* information listed above is at the time of submission.

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