An Integrated Modeling and Fault Simulation Environment for Analyzing Aircraft Subsystem Interactions

Award Information
Agency: Department of Defense
Branch: Navy
Contract: N68335-04-C-0022
Agency Tracking Number: N022-0937
Amount: $750,000.00
Phase: Phase II
Program: SBIR
Awards Year: 2003
Solitcitation Year: N/A
Solitcitation Topic Code: N/A
Solitcitation Number: N/A
Small Business Information
125 Tech Park Drive, Rochester, NY, 14623
Duns: 073955507
Hubzone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Michael Roemer
 Director of Engineering
 (585) 424-1990
Business Contact
 Mark Redding
Title: President
Phone: (585) 424-1990
Research Institution
Impact Technologies, in cooperation with the Honeywell F-35 PTMS development team, propose the development, customization and implementation of a software simulation environment specifically focused on the integrated modeling of the F-35 PTMS (PowerThermal Management System), but can be applied across various vehicle subsystems. The proposed fault simulation and analysis test bench will be used to rigorously evaluate the failure mode interactions between all LRU and subsystems of systems such as thePTMS. The integrated software simulation demonstrated in Phase I within the Matlab/Simulink software will be further developed and applied to the F-35 PTMS with capability of failure mode modeling, full dynamic simulation, functional subsysteminteraction, and provide PHM algorithm interface

* information listed above is at the time of submission.

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