On the Dynamical Properties of the Sun-Earth-Moon Restricted Four Body Problem

Article Preview

Abstract:

The properties of the sun-earth-moon restricted four body problem were investigated. On the base of the earth-moon circular restricted three body problem, taking gravitation effect of the sun into account, a dynamic model of restricted four body problem was established. Equilibrium points were calculated by proper numerical method and linearization procedure was introduced to obtain the stability of these points. An invariant integral relation of this four body problem similar with Jacobi integral was derived, then the Hill region was investigated. Calculation results show that the equilibrium points will keep moving near libration points, also has their stability unchanged, and the Hill region will be non-periodically time varying.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 834-836)

Pages:

1869-1872

Citation:

Online since:

October 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] C. Simo, G. Gomez, A. Jorba, et al, in: From Newton to Chaos, edited by Roy A E, Steves B A., Plenum Press, New York (1995).

Google Scholar

[2] K. Yagasaki: Celestial Mechanics and Dynamical Astronomy Vol. 90 (2004), p.197.

Google Scholar

[3] K. Yagasaki: Physica D Vol. 197 (2004), p.313.

Google Scholar

[4] M.A. Andreu: The quasi-bicircular problem (Universitat de Barcelona, Spain 1998).

Google Scholar

[5] M.A. Andreu: Celestial Mechanics and Dynamical Astronomy Vol. 84 (2002), p.105.

Google Scholar

[6] K.C. Howell, D.B. Spencer: Acta Astronautica Vol. 13 (1986), p.473.

Google Scholar

[7] L.G. Luk'yanov: Astronomy Reports Vol. 1 (2005), p.1018.

Google Scholar