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A procedure for calculating the damping in multi-element space structuresA procedure for analyzing the damping in a multielement space structure connected by joints is described, in which distributed material damping and discrete nonlinear joint properties are incorporated into a linear analysis. The procedure involves four steps: (1) creation of a linear undamped finite element model; (2) experimental measurements of the transient response of a truss member in free fall tests to obtain material damping properties; with these properties incorporated into a linear damped finite element model of the structure; (3) the identification of the nonlinear joint properties using the force-state mapping technique; and (4) linearization of the identified nonlinear components, which are then incorporated into the linear damped model to create the linearized damped finite element model.
Document ID
19870028657
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crawley, E. F.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Odonnell, K. J.
(MIT Cambridge, MA, United States)
Date Acquired
August 13, 2013
Publication Date
October 1, 1986
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 86-203
Report Number: IAF PAPER 86-203
Accession Number
87A15931
Funding Number(s)
CONTRACT_GRANT: NAGW-21
Distribution Limits
Public
Copyright
Other

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