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Analytical performance prediction for large antennasThe coupled free-free modes of the 55M LMSS antenna configuration are shown. They were determined using modal synthesis. Reflector modes clamped at the hub were calculated adopting the efficient cyclic symmetry technique. Similarly, clamped hub modes of the offset boom structure were calculated. The modes of the two substructures were then combined through the process of modal synthesis on the assumption that the interface at the hub structure is rigid thus satisfying statically determinate matching conditions. For attitude control purposes, only modes associated with symmetric components zero and one involve net motions of the center of gravity of the reflector. This condition restricts the set of admissible eigenfunctions for modal synthesis. Modes with symmetric components higher than one are excited only by forces acting on the ribs. These modes are totally uncoupled from the boom dynamics.
Document ID
19820011386
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
El-Raheb, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Langley Research Center Large Space Systems Technol., Pt. 2, 1981
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
82N19260
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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