Parametric oscillations of a deformable spacecraft

Details Parametric oscillations of a deformable spacecraft Parametric oscillations of a deformable spacecraft

Mar 1992

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992kosis..30..275s&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 30, no. 2, Mar.-Apr. 1992, p. 275-278. In Russian.

Physics

Elastic Deformation, Spacecraft Structures, Structural Vibration, Dynamic Structural Analysis, Eigenvectors, Elastic Bodies

Scientific paper

A theoretical analysis of the parametric oscillations of a deformable
spacecraft is presented. The spacecraft is represented as a dynamically
symmetric mechanical system consisting of an elastic part and a rigid
part. The elastic part is subjected to a pulsating load.

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