On the equatorial orbits of a satellite of a triaxial attracting rigid body

Details On the equatorial orbits of a satellite of a triaxial attracting rigid body On the equatorial orbits of a satellite of a triaxial attracting rigid body

Jan 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983kosis..21..128s&link_type=abstract

Kosmicheskie Issledovaniia, vol. 21, Jan.-Feb. 1983, p. 128-131. In Russian.

Physics

Celestial Mechanics, Equatorial Orbits, Orbit Calculation, Axes Of Rotation, Ellipsoids, Gravitational Fields, Rigid Structures, Rotating Bodies

Scientific paper

The paper examines the motion of a satellite in the gravitational field of a rigid body with a triaxial central ellipsoid of inertia rotating uniformly about the smallest axis of the ellipsoid of inertia. A model problem is developed for investigating the motion of an equatorial satellite of a slowly rotating triaxial body and a satellite with a small orbital inclination to the equatorial plane.

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