Hybrid systems for use in the dynamics of artificial satellitesThe paper discusses the advantages and disadvantages of adopting either an inertial or a noninertial reference system for computing the orbital elements of artificial satellites. The effects of precession and nutation are examined, and determination of disturbing functions is explained for both an inertial and a noninertial system.
Document ID
19760034275
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Kozai, Y. (Tokyo Astronomical Observatory, Mitaka, Japan; Smithsonian Astrophysical Observatory and Harvard College Observatory, Cambridge Mass., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Subject Category
Astrodynamics
Meeting Information
Meeting: On reference coordinate systems for earth dynamics