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Multiple degree of freedom force-state component identificationForce-state mapping is extended to allow the quasistatic characterization of realistic multiple degree of freedom systems whose constitutive relations are nonlinear, dissipative, coupled and depend on memory of past states. A general constitutive force-state model is formulated, which includes dynamic hysteresis phenomena typical of that found in deployable structures. A two step parameter identification approach is developed, which employs a linear extended Kalman filter and a nonlinear least squares fit. A six degree of freedom force-state testing device was constructed, and used to obtain data on one bay of a simple truss and on one bay of the MODE deployable truss.
Document ID
19930050182
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Masters, Brett P.
(NASA Langley Research Center Hampton, VA, United States)
Crawley, Edward F.
(MIT Cambridge, MA, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA(ASME)ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 34th and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pt. 5 (A93-33876 1
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 93-1654
Accession Number
93A34179
Funding Number(s)
CONTRACT_GRANT: NAS1-18690
CONTRACT_GRANT: NAGW-1335
Distribution Limits
Public
Copyright
Other

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