Abstract

We prove new variational properties of the spatial isosceles orbits in the equal-mass three-body problem and analyze their linear stabilities in both the full phase space \begin{document}$\mathbb{R}^{12}$\end{document} and a symmetric subspace Γ. We prove that each spatial isosceles orbit is an action minimizer of a two-point free boundary value problem with non-symmetric boundary settings. The spatial isosceles orbits form a one-parameter set with rotation angle θ as the parameter. This set of orbits always lies in a symmetric subspace Γ and we show that their linear stabilities in the full phase space \begin{document}$\mathbb{R}^{12}$\end{document} can be simplified to two separated sub-problems: linear stabilities in Γ and \begin{document}$(\mathbb{R}^{12} \setminus Γ) \cup \{0\}$\end{document} . By applying Roberts' symmetry reduction method, we prove that the orbits are always unstable in the full phase space \begin{document}$\mathbb{R}^{12}$\end{document} , but it is linearly stable in Γ when \begin{document}$θ ∈ [0.33π, 0.48 π] \cup [0.52 π, 0.78 π]$\end{document} .

Highlights

  • Recall thatQ(2) = Qstart · RF (θ) = −(a1 + a2) cos 2θ −(a1 + a2) sin 2θ 0

  • Introduction and main resultsIn this paper, we study the variational existence and the linear stability of spatial isosceles orbits in the equal-mass three-body problem

  • We show that the spatial isosceles orbit is an action minimizer of a two-point free boundary value problem in χ under non-symmetric boundary settings

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Summary

Recall that

Q(2) = Qstart · RF (θ) = −(a1 + a2) cos 2θ −(a1 + a2) sin 2θ 0 It follows that paths P−1 and P2 are both connected to P0 at t = 0 and t = 1 respectively. By applying the uniqueness of solution of ODE system, Lemma 3.3 imply that the connected path PPP = P−1 ∪ P0 ∪ P2 is a smooth path and so PPP is a solution of the Newtonian equations in the three-body problem. It implies that a10 = −a20 in Qstart and the minimizer P0 coincides with P0, which is the spatial isosceles orbit.

Since the spatial isosceles orbit is in the subspace
Then in its linearized equation dξ dt
The equations of motion in these variables are dr dt
The period T of the periodic solution is
Choose the third column of a
By the choice of the matrix
We compute d

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