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NASA NTRS ยท 19850010920

Condensed Antenna Structural Models for Dynamics Analysis

Abstract

Condensed degree-of-freedom models are compared with large degree-of-freedom finite-element models of a representative antenna-tipping and alidade structure, for both locked and free-rotor configurations. It is shown that: (1) the effective-mass models accurately reproduce the lower-mode natural frequencies of the finite element model; (2) frequency responses for the two types of models are in agreement up to at least 16 rad/s for specific points; and (3) transient responses computed for the same points are in good agreement. It is concluded that the effective-mass model, which best represents the five lower modes of the finite-element model, is a sufficient representation of the structure for future incorporation with a total servo control structure dynamic simulation.

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BibTeXRIS

Levy, R.. 1985-02-15. Condensed Antenna Structural Models for Dynamics Analysis. https://ntrs.nasa.gov/citations/19850010920

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