Experimental determination of the coefficients of the equations of the perturbed motion of a spacecraft with elastic elements

Details Experimental determination of the coefficients of the equations of the perturbed motion of a spacecraft with elastic elements Experimental determination of the coefficients of the equations of the perturbed motion of a spacecraft with elastic elements

Sep 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990kosis..28..685a&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 28, Sept.-Oct. 1990, p. 685-691. In Russian.

Physics

Elastic Bodies, Flexible Spacecraft, Orbit Perturbation, Rigid Structures, Satellite Perturbation, Spacecraft Motion, Equations Of Motion, Free Vibration, Structural Vibration

Scientific paper

Attention is given to experimental methods for determining the
inertial-coupling coefficients and dissipative coefficients of equations
describing the perturbed motion of a spacecraft consisting of a rigid
body and elastic elements. These elements can be solar panels or
instrumentation booms.

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