No CrossRef data available.
Article contents
Analytical Effects of Gravitational Waves on the Motion of an Artificial Satellite
Published online by Cambridge University Press: 12 April 2016
Abstract
Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.
The motion of an artificial satellite in the Earth’s gravitational field is discussed in the post-Newtonian framework including the effect of weak gravitation waves using the perturbation technique of the canonical Lie-transformations. Two successive canonical transformations are used to derive analytical expressions for the short-period, long-period and secular perturbations of orbital elements. The solution is expressed in terms of the Delaunay variables.
- Type
- Theory of Motion
- Information
- Copyright
- Copyright © Kluwer 1997
References
Brouwer, D.: 1959, “Solution of the problem of artificiad satellite theory without Drag”, Astron. J.
64, 378.Google Scholar
Deprit, A.: 1969, “Canonical transformations depending on a small parameter”, Celest. Mech.
1, 12.Google Scholar
Heimberger, J., Soffel, M., and Ruder, H.: 1990, “Relativistic effects in the motion of artificial satellites: The oblateness of the central body H”, Celest. Mech.
47, 205.Google Scholar
Hori, G.: 1966, “Theory of general perturbations with unspecified canonical variables”, Publ. Astron. Soc. Jpn.
18, 287.Google Scholar
Soffel, M., Wirrer, R., Schastok, J., Ruder, H. and Schneider, M.: 1988, “Relativistic effects in the motion of artificial satellites: The oblateness of the central body. I”, Celest. Mech.
42, 81.Google Scholar
Straumann, N.: 1984
General Relativity and Relativistic Astrophysics, Springer, Berlin.Google Scholar
Youssef, M.: 1994, The effect of Gravitational Waves on the Motion of Artificial Satellites, Ph.D. thesis, Astronomy Dept., Cairo University, Egypt.Google Scholar