Transition to chaos in the planar, circular, restricted three body problem is investigated. In particular, a model Hamiltonian suitable for the description of the motion of the asteroid Ceres is introduced. The break-down threshold of invariant surfaces (nearby the position of Ceres in phase space) is computed by means of different numerical methods, which allow to detect the transition from regular to chaotic motion. The experiments show that in the proximity of the location of the asteroid, invariant surfaces cease to exist for a mass ratio (between the perturbing body, Jupiter and the primary, the Sun) between 0.002 and 0.004. We remind that the real value of the above mass ratio is about 0.001 as derived from astronomical observations.

Celletti, A., Froeschle', C. (1998). Numerical investigation of the break-down threshold for a restricted three-body problem. PLANETARY AND SPACE SCIENCE, 46(11-12), 1535-1542 [10.1016/S0032-0633(98)00056-7].

Numerical investigation of the break-down threshold for a restricted three-body problem

CELLETTI, ALESSANDRA;
1998-01-01

Abstract

Transition to chaos in the planar, circular, restricted three body problem is investigated. In particular, a model Hamiltonian suitable for the description of the motion of the asteroid Ceres is introduced. The break-down threshold of invariant surfaces (nearby the position of Ceres in phase space) is computed by means of different numerical methods, which allow to detect the transition from regular to chaotic motion. The experiments show that in the proximity of the location of the asteroid, invariant surfaces cease to exist for a mass ratio (between the perturbing body, Jupiter and the primary, the Sun) between 0.002 and 0.004. We remind that the real value of the above mass ratio is about 0.001 as derived from astronomical observations.
1998
Pubblicato
Rilevanza internazionale
Articolo
Esperti anonimi
Settore MAT/07 - FISICA MATEMATICA
English
Celletti, A., Froeschle', C. (1998). Numerical investigation of the break-down threshold for a restricted three-body problem. PLANETARY AND SPACE SCIENCE, 46(11-12), 1535-1542 [10.1016/S0032-0633(98)00056-7].
Celletti, A; Froeschle', C
Articolo su rivista
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/2108/94953
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