Systems of artificial earth satellites in stable circular diurnal orbits

Details Systems of artificial earth satellites in stable circular diurnal orbits Systems of artificial earth satellites in stable circular diurnal orbits

Jan 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983kosis..21...12v&link_type=abstract

Kosmicheskie Issledovaniia, vol. 21, Jan.-Feb. 1983, p. 12-19. In Russian.

Physics

Circular Orbits, Earth Orbits, Orbital Elements, Satellite Networks, Satellite Perturbation, Spacecraft Stability, Canonical Forms, Equations Of Motion, Long Term Effects, Orbital Mechanics, Satellite Orbits, Three Body Problem

Scientific paper

The paper examines the problem of determining the initial parameters of the motion of a system of satellites in almost-circular orbit, these parameters determining the orbital stability of individual satellites and the stability of the angular distance between a pair of satellites over a number of years. An example of such systems is a system consisting of three satellites in orbits with initial inclinations of 48 and 43 deg. The stability of these orbits over a period of five years is investigated.

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