NASA NTRS · 19870031213
Parameter identification in distributed spacecraft structures
Abstract
This paper develops a new technique for the identification of parameters in distributed systems. The technique is based on the finite element method. An an illustration, the method is applied to the identification of the mass and stiffness distributions of a space structure, simulated by a nonuniform free-free beam.
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Meirovitch, L., Norris, M. A.. 1986-01-01. Parameter identification in distributed spacecraft structures. https://ntrs.nasa.gov/citations/19870031213
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