Canonical variables and canonical integrals for motion in nearly circular orbits

Details Canonical variables and canonical integrals for motion in nearly circular orbits Canonical variables and canonical integrals for motion in nearly circular orbits

May 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987kosis..25..393n&link_type=abstract

Kosmicheskie Issledovaniia (ISSN 0023-4206), vol. 25, May-June 1987, p. 393-399. In Russian.

Physics

Canonical Forms, Circular Orbits, Equations Of Motion, Independent Variables, Integrals, Spacecraft Orbits, Navigation, Orbit Calculation

Scientific paper

The motion of a spacecraft in a nearly circular orbit is divided into
motions in three independent subspaces. These subspaces have their own
variables and integrals of motion, which are used for the analytical
solution of problems of optimal navigation and orbit correction.

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