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Technical Papers

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Portfolio // Technical Papers

ATA has been a leader in methods development for design, analysis, and test for more than 45 years.

As a result of this experience, ATA regularly produces technical papers and presents at conferences. Our
technical papers draw on our vast industry experience and cover topics in all areas of ATA business. Learn
more about our work by requesting a technical paper.
Rezayat, M. An Introduction to Computer Agents and Their Applications. Mohsen’s Seminar, Feb 1997.
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Rezayat, M. I-DEAS/Metaphase Data Server/Publisher. Mohsen’s Seminar, Feb 1997.
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Smith, K., and C. Peng. Mars Pathfinder Entry, Descent, and Landing System: Design Concept and Simulation of System Dynamics. 14th Aerodynamic Decelerator Systems Technology Conference, San Francisco, CA, Jun 1997.
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Smith, K.S., and C. Peng. Air Mass Effects on the Cassini High Gain Antenna. IMAC XV, 1997.
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Stokes, W., J. Bretl, A. Crewe, W.S. Park, J.Y. Lee, and M.S. Lee. Computer Simulation of In-Vehicle Boom Noise. SAE Noise and Vibration Conference, Traverse City, MI, May 1997.
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Vold, H., H. Herlufsen, M. Mains, and D. Corwin-Renner. Multi Axle Order Tracking with the Vold-Kalman Tracking Filter. Sound and Vibration, 1997.
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Blades, E. L., and R. R. Craig, Jr. A Frequency-Domain Substructure System Identification Algorithm. Aug 1996.
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Brillhart, R., D. Hensley, and M. Stabb. Pegasus XL FIN Dynamic Characterization for Flutter Evaluation. 14th International Modal Analysis Conference, Dearborn, MI, Feb 1996.
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Brillhart, R., D. Hensley, and R. LeBlanc. Gulfstream V Ground Vibration Test – Aid in Concurrent Engineering. 14th IMAC, Dearborn, MI, Feb 1996.
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Brillhart, R., D. Hensley, M. Stabb, and R. Pinkham Pegasus XL Fin Dynamic Characterization for Flutter Evaluation. IMAC 1996.
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Craig, R. R., Jr., and E. L. Blades. Substructure System Identification-Reduced Order Models. 3rd International Conference on Dynamics and Control of Structures in Space, Cranfield, England, 1996.
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Craig, R., Jr., E. Blades, and W. Cutshall. A Reduced-Order Substructure System Identification Method. AIAA-1996-1200. Dynamics Specialists Conference, 1996.
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Dillon, M., B. Fladung, and D. Brown. Improved Impact Testing Throughput by Using a 3D Digitizing System. International Modal Analysis Conference, 1996.
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Fladung, W.A., and R.W. Rost. Cause and Effect of Applying the Exponential Window to an Impact Force Signal. International Modal Analysis Conference, 1996.
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Flanigan, C., M. Stabb, and R. Pinkham. Aeroelastic Design and Analysis of Winged Launch Vehicles. AIAA Dynamics Specialists Conference, Salt Lake City, UT, Apr 18-19, 1996.
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Redcay, J. CAD Comes to Cycling. Apr 1996.
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Stabb, M., R. Brillhart, C. Flanigan, and R. Pinkham. Aeroelastic Analysis and Test of the Pegasus XL Launch Vehicle. 16th Aerospace Testing Seminar, Manhattan Beach, CA, Mar 12-14, 1996.
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Antal, G., R. Brillhart, D. Hensley, and L. Freudinger. Implementation of an Automated Approach for Spatial Filtering of Flight Flutter Test Data. 1995.
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Blelloch, P.A., and M.C. Stabb. Selecting Accelerometer Locations Using Flexibility Shapes. 1995.
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Bretl, J. Advancements in Computer Simulation Methods for Vehicle Noise and Vibration. SAE Noise and Vibration Conference, Traverse City, MI, May 1995.
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George M. Low Award Recipient

ATA is a proud recipient of the prestigious George M. Low award, NASA’s premier quality
and performance award recognizing contractors for technical and business excellence.

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