Generalized Analytical Results on n-Ejection–Collision Orbits in the RTBP. Analysis of Bifurcations
In the planar circular restricted three-body problem and for any value of the mass parameter μ ∈ ( 0 , 1 ) and n ≥ 1 , we prove the existence of four families of n -ejection–collision ( n -EC) orbits, that is, orbits where the particle ejects from a primary, reaches n maxima in the (Euclidean) dista...
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Veröffentlicht in: | Journal of nonlinear science 2023-02, Vol.33 (1), Article 17 |
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Sprache: | eng |
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Zusammenfassung: | In the planar circular restricted three-body problem and for any value of the mass parameter
μ
∈
(
0
,
1
)
and
n
≥
1
, we prove the existence of four families of
n
-ejection–collision (
n
-EC) orbits, that is, orbits where the particle ejects from a primary, reaches
n
maxima in the (Euclidean) distance with respect to it and finally collides with the primary. Such EC orbits have a value of the Jacobi constant of the form
C
=
3
μ
+
L
n
2
/
3
(
1
-
μ
)
2
/
3
, where
L
>
0
is big enough but independent of
μ
and
n
. In order to prove this optimal result, we consider Levi-Civita’s transformation to regularize the collision with one primary and a perturbative approach using an ad hoc small parameter once a suitable scale in the configuration plane and time has previously been applied. This result improves a previous work where the existence of the
n
-EC orbits was stated when the mass parameter
μ
>
0
was small enough. Moreover, for decreasing values of
C
, there appear some bifurcations which are first numerically investigated and afterward explicit expressions for the approximation of the bifurcation values of
C
are discussed. Finally, a detailed analysis of the existence of
n
-EC orbits when
μ
→
1
is also described. In a natural way, Hill’s problem shows up. For this problem, we prove an analytical result on the existence of four families of
n
-EC orbits, and numerically, we describe them as well as the appearing bifurcations. |
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ISSN: | 0938-8974 1432-1467 |
DOI: | 10.1007/s00332-022-09873-y |