2005A&A...437..333O

Query : 2005A&A...437..333O

2005A&A...437..333O - Astronomy and Astrophysics, volume 437, 333-338 (2005/7-1)

A simple intermediary orbit for the J2 problem.

OBERTI P.

Abstract (from CDS):

A simple precessing ellipse suitable for satellites with moderate eccentricities and inclinations is built in the Hamiltonian context of the J2 problem. Easy to use as a first intermediary orbit, it provides a substantially closer starting point for series expansions than the regular Keplerian ellipse.

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Journal keyword(s): planets and satellites: general - celestial mechanics

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