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Identification of Nonlinear Micron-Level Mechanics for a Precision Deployable JointThe experimental identification of micron-level nonlinear joint mechanics and dynamics for a pin-clevis joint used in a precision, adaptive, deployable space structure are investigated. The force-state mapping method is used to identify the behavior of the joint under a preload. The results of applying a single tension-compression cycle to the joint under a tensile preload are presented. The observed micron-level behavior is highly nonlinear and involves all six rigid body motion degrees-of-freedom of the joint. it is also suggests that at micron levels of motion modelling of the joint mechanics and dynamics must include the interactions between all internal components, such as the pin, bushings, and the joint node.
Document ID
19970001795
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Bullock, S. J.
(Colorado Univ. Boulder, CO United States)
Peterson, L. D.
(Colorado Univ. Boulder, CO United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Mechanical Engineering
Report/Patent Number
AIAA Paper 94-1347-CP
NASA-CR-202597
NAS 1.26:202597
Report Number: AIAA Paper 94-1347-CP
Report Number: NASA-CR-202597
Report Number: NAS 1.26:202597
Accession Number
97N11566
Funding Number(s)
CONTRACT_GRANT: NAGw-1388
CONTRACT_GRANT: NAG1-1490
Distribution Limits
Public
Copyright
Public Use Permitted.
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