The Main Problem in Satellite Theory Revisited

Details The Main Problem in Satellite Theory Revisited The Main Problem in Satellite Theory Revisited

Mar 2000

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2000cemda..76...79h&link_type=abstract

Celestial Mechanics and Dynamical Astronomy, Volume 76, Issue 2, pp.79-120

Astronomy and Astrophysics

Astronomy

2

Lie Transformation, Normal Form, Closed Form, Computer Algebra

Scientific paper

Using the elimination of the parallax followed by the Delaunay normalization, we present a procedure for calculating a normal form of the main problem ( J 2 perturbation only) in satellite theory. This procedure is outlined in such a way that an object-oriented automatic symbolic manipulator based on a hierarchy of algebras can perform this computation. The Hamiltonian after the Delaunay normalization is presented to order six explicitly in closed form, that is, in which there is no expansion in the eccentricity. The corresponding generating function and transformation of coordinates, too lengthy to present here to the same order; the generator is given through order four.

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