Mathematics
Scientific paper
Jan 1980
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1980kosis..18...38i&link_type=abstract
Kosmicheskie Issledovaniia, vol. 18, Jan.-Feb. 1980, p. 38-44. In Russian.
Mathematics
Mathematical Models, Orbital Mechanics, Satellite Perturbation, Spacecraft Motion, Angular Velocity, Atmospheric Attenuation, Elliptical Orbits, Qualitative Analysis, Quantitative Analysis, Spacecraft Structures
Scientific paper
An equivalent perturbation model is developed for the analytical study of effect of the principal perturbing factors on the qualitative structure of the relative motion of a spacecraft in the case of constant angular velocity of the line of sight. Quantitative determinations are made which make it possible to evaluate changes of system structure owing to orbit ellipticity, relative range, and atmospheric drag.
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