Generalized intermediary potentials for satellite orbits around oblate planets

Authors

  • Vladimir Martinusi Technion – Israel Institute of Technology, Faculty of Aerospace Engineering, Israel

Keywords:

main problem in artificial satellite theory, intermediary potential, radial intermediary, zonal intermediary, perturbation theory, gravitational, potential

Abstract

The main problem in artificial satellite theory is modeled by an initial value problem describing the motion of a mass particle in an axially symmetric potential. In the case of Earth, this potential is truncated up to order 4 in the series that approximate the full potential, and only the even zonal harmonics terms are considered. The problem is non-integrable and even exhibits chaotic behaviour. However, approximate solutions may be given by replacing the original potential with an approximation, generally named an intermediary potential. Several solutions have been offered in this way starting from the beginning of the space era at the middle of the 20th century. The present work offers the general intermediary potential that contains all of the previous models as particular cases, opening the path in finding the most appropriate potential for various types of orbits.

References

AKSNES, K., On the dynamical theory of a near-earth satellite, I., Astrophysica Norvegica, 10, p. 69, 1965.

BROUWER, D., Solution of the problem of artificial satellite theory without drag, Astronomical Journal, 64, p. 378, 1959.

CID, R., LAHULLA, J.F., Perturbaciones de corto periodo en el movimiento de un satelite artificial, en funcion de las variables de Hill, Publicaciones de la Revista de la Academia de Ciencias de Zaragoza, 24, p. 159, 1969.

DEPRIT, A., The elimination of the parallax in satellite theory, Celestial Mechanics, 24, 2, pp. 111-153, 1981.

DEPRIT, A., Canonical transformations depending on a small parameter, Celestial Mechanics, 1, 1, pp. 12-30, 1969.

FERRANDIZ, J.M., FLORIA, L., Towards a systematic definition of intermediaries in the theory of artificial satellites, Bulletin of the Astronomical Institutes of Czechoslovakia, 42, pp. 401-407, 1991.

GARFINKEL, B., On the motion of a satellite of an oblate planet, Astronomical Journal, 63, p. 88, 1958.

GARFINKEL, B., The orbit of a satellite of an oblate planet, Astronomical Journal, 64, p. 353, 1959.

GURFIL, P., LARA, M., Satellite onboard orbit propagation using Deprit’s radial intermediary, Celestial Mechanics and Dynamical Astronomy, 120, pp, 217–232, 2014.

LYDDANE, R.H., Small eccentricities or inclinations in the Brouwer theory of the artificial satellite, Astronomical Journal, 68, p. 555, 1963.

STERNE, T.E., The gravitational orbit of a satellite of an oblate planet, Astronomical Journal, 63, p. 28, 1958.

Published

2020-12-10