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Analytical and Simulation Framework for Performance Validation of Complex Systems

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNL04AC31P
Agency Tracking Number: 034619
Amount: $69,984.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: A7.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2003
Award Year: 2004
Award Start Date (Proposal Award Date): 2004-01-16
Award End Date (Contract End Date): 2004-07-19
Small Business Information
1160 Pepsi Place, Suite300
Charlottesville, VA 22901-0807
United States
DUNS: 120839477
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Alec Bateman
 Principal Investigator
 (434) 973-1215
 bateman@barron-associates.com
Business Contact
 David Ward
Title: Business Official
Phone: (434) 973-1215
Email: barron@barron-associates.com
Research Institution
N/A
Abstract

To remain competitive, the US aerospace industry must continually improve system performance (e.g. increased adaptation and autonomy), enhance safety (e.g., fault tolerant systems), and reduce costs. These improvements demand avionics software that is orders of magnitude more complex than that used in current operational systems. While software complexity is increasing, there is a tremendous (and appropriate) pressure to ensure that new designs are safer to operate than the simpler systems they replace. In many cases (e.g., damage-adaptive control), methods that can improve vehicle performance are not used because verification and validation (V&V) tools that help ensure the complex system will not behave in an unexpected way are not available. The proposed research will lay the groundwork for such a tool by building on prior work by the authors in four unique areas: (1) the tool will work in the MATLAB/Simulink environment and will be easy to set up and operate, (2) the tool will be modular and allow easy integration of a variety of closed-form analysis methods, (3) the tool will aid in evaluating system performance as well as stability, and (4) the tool will assist in piloted simulation and flight test design.

* Information listed above is at the time of submission. *

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