MULTIPLE DEGREE-OF-FREEDOM FORCE-STATE COMPONENT IDENTIFICATION

Citation
Bp. Masters et Ef. Crawley, MULTIPLE DEGREE-OF-FREEDOM FORCE-STATE COMPONENT IDENTIFICATION, AIAA journal, 32(11), 1994, pp. 2276-2285
Citations number
14
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
32
Issue
11
Year of publication
1994
Pages
2276 - 2285
Database
ISI
SICI code
0001-1452(1994)32:11<2276:MDFCI>2.0.ZU;2-I
Abstract
Force-state mapping is extended to allow the quasistatic characterizat ion of realistic multiple degree-of-freedom systems whose constitutive relations are nonlinear, dissipative, coupled, and depend on memory o f 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 least squares and a nonlin ear least squares fit. A six degree-of-freedom force-state testing dev ice was constructed and used to obtain data on one bay of a simple tru ss and on one bay of the mid-deck 0-gravity dynamics experiment deploy able truss.