Technical Papers

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ATA has been a leader in methods development for design, analysis, and test for more than 40 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.

Lindenmoyer, A., and J. Habermeyer. An Automated, Integrated Approach to Space Station Structural Modeling. 30th Structures, Structural Dynamics, and Materials Conference, Mobile, AL, Apr 1989.
O’Callahan, J. A Procedure for an Improved Reduced System (IRS) Model. 7th International Modal Conference, Las Vegas, NV, 1989.
Rezayat, M. Fast Decomposition of Matrices Generated by the Boundary Element Method. 6th International Conference on Numerical Methods in Thermal Problems, Swansea, Wales, UK, Jul 1989.
Baker, M., and P. Blelloch. Space Station Dynamic Analysis Methods. 5th IMAC, London, April 1987.
Brillhart, R., and G. Thomas. The Design of a Space Optical System Using Computer Aided Engineering Techniques Structural Mechanics of Optical Systems II. Proceedings of SPIE – The International Society for Optical Engineering, Los Angeles, CA, Jan 1987.
Conti, P., and J. Bretl. Determination of Mount Stiffnesses and Inertia Properties From Modal Test Data. Modal Testing and Analysis DE-Vol. 3, Proceedings of ASME Design Technology Conference, Boston, MA, Sep 1987.
Conti, P., and J. Bretl. Rigid Body Mass Properties from Test Data. Proceedings of 5th International Modal Analysis Conference, London, Apr 1987.
Baker, M., H. Chiger, J.A. Habermeyer, P.J. Hipol, C.L. Johnson, and L.J. DeRyder. Space Station Multidisciplinary Analysis Capability — IDEAS. 27th Structures, Structural Dynamics and Materials Conference, San Antonio, TX, May 1986.
Frantz, J., D.C. Kammer, M. Baker, and S. Pincura. Shock and Vibration Analysis of a Communication System Subject to Nuclear Blast. MILCOM 86 Conference, 1986.
Garbo, S.P., S.W. Hong, and W. Kim. Strength Evaluation of Helicopter Composite Bolted Joints. 27th Structures, Structural Dynamics and Materials Conference, May 19-21, 1986.
Kammer, D.C., and M. Baker. A Comparison of the Craig-Bampton and Residual Flexibility Methods of Substructure Representation. 26th Structures, Structural Dynamics, and Materials Conference, Orlando, FL, April 1985.

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