Evolution of singular elliptic orbits of synchronous spacecraft.

Details Evolution of singular elliptic orbits of synchronous spacecraft. Evolution of singular elliptic orbits of synchronous spacecraft.

Jul 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991cosre..29..123v&link_type=abstract

Cosmic Res., Vol. 29, No. 1, p. 123 - 133

Computer Science

Artificial Satellites: Orbital Evolution

Scientific paper

A class of elliptic spacecraft orbits is studied whose period of revolution is close to a day, inclined at approximately 60°, of eccentricity 0.5 - 0.8 and with argument of perigee latitude ±90°. From a system of equations of motion, linearized around the singular solution of the Hill problem, taking into account the compression of the planet, the author obtains the dependences of the spacecraft's orbital elements on time, giving a satisfactory description of their variation on an interval of the order of five years.

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