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Eigensensitivity analysis for space structures with applications in design optimizationAn approximate structural eigenvalue/vector analysis technique which uses eigensensitivities in a truncated Taylor series expression is presented. It is shown that this technique can provide the computational efficiency urgently needed for large scale control-structure optimization problems. In addition, a unified formulation and solution approach for calculating eigenvalue and eigenvector derivatives of the real symmetric structural eigenvalue problem is presented.
Document ID
19930068893
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kenny, Sean P.
(NASA Langley Research Center Hampton, VA, United States)
Hou, Gene J.
(Old Dominion Univ. Norfolk, VA, United States)
Belvin, W. K.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
October 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Shock and Vibration Symposium
Location: Pasadena, CA
Country: United States
Start Date: October 16, 1990
End Date: October 18, 1990
Accession Number
93A52890
Distribution Limits
Public
Copyright
Other

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