This paper analyzes the linear stability of elliptic relative equilibria in a restricted four-body problem with three primaries forming a Lagrangian triangle, revealing stability regions based on mass parameters and eccentricity.
Contribution
It provides a comprehensive bifurcation diagram for stability regions, employing $ ext{om}$-Maslov index and differential operator theories, and identifies two stable sub-regions.
Findings
01
Full bifurcation diagram of stability regions
02
Identification of two stable sub-regions
03
Dependence of stability on mass parameters and eccentricity
Abstract
In this paper, we consider the linear stability of the elliptic relative equilibria of the restricted 4-body problems where the three primaries form a Lagrangian triangle. By reduction, the linearized Poincar\'e map is decomposed to the essential part, the Keplerian part and the elliptic Lagrangian part where the last two parts have been studied in literature. The linear stability of the essential part depends on the masses parameters α, β with α≥β>0 and the eccentricity e∈[0,1). Via \om-Maslov index theory and linear differential operator theory, we obtain the full bifurcation diagram of linearly stable and unstable regions with respect to α, β and e. Especially, two linearly stable sub-regions are found.
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Full text
Linear Stability of Elliptic Relative Equilibria of
Restricted Four-body Problem
Bowen Liu1, Qinglong Zhou2,
1 Institut für Mathematik
Universität Augsburg, D-86135 Augsburg, Germany
2 Department of Mathematics
Zhejiang University, Hangzhou 310027, Zhejiang, China
Partially supported by NSFC (No. 11131004, No. 11671215) and Sino-German (CSC-DAAD) Postdoc Scholarship Program (CSC No. 201800260010 and DAAD No. 91696544) funded by China Scholarship Council and Deutscher Akademischer Austausch Dienst.
E-mail: [email protected] supported by the Natural Science Foundation of Zhejiang Province (No. Y19A010072) and the Fundamental Research Funds for the Central Universities (No. 2019QNA3002).
E-mail: [email protected]
Abstract
In this paper, we consider the linear stability of the elliptic relative equilibria of the restricted 4-body problems where the three primaries form a Lagrangian triangle.
By reduction, the linearized Poincaré map is decomposed to the essential part, the Keplerian part and the elliptic Lagrangian part where the last two parts have been studied in literature.
The linear stability of the essential part depends on the masses parameters
α, β with α≥β>0 and the eccentricity e∈[0,1).
Via ω-Maslov index theory and linear differential operator theory, we obtain the full bifurcation diagram of linearly stable and unstable regions with respect to α, β and e. Especially, two linearly stable sub-regions are found.
Keywords: restricted planar four-body problem, Lagrangian solutions, linear stability, ω-index theory,
perturbations of linear operators.
AMS Subject Classification: 58E05, 37J45, 34C25
1 Introduction and main results
Let q1,q2,…,qn∈R2 be the position vectors of n particles with masses m1, m2, …, mn>0 respectively.
By the law of universal
gravitation and Newton’s second law,
the system of equations is
[TABLE]
where U(q)=U(q1,q2,…,qn)=∑1≤i<j≤n∣qi−qj∣mimj is the
potential or force function by using the standard norm ∣⋅∣ of vector in R2.
Letting pi=miq˙i∈R2 for 1≤i≤n, then (1.1) is transformed to a Hamiltonian system
[TABLE]
with Hamiltonian function
[TABLE]
A central configuration(q1,q2,…,qn)=(a1,a2,…,an) is a solution of
[TABLE]
for some constant λ.
A direct computation shows that λ=2I(a)U(a)>0,
where I(a)=21∑mi∣ai∣2 is the moment of inertia.
Readers may refer [28] and [34] for the properties of central configuration.
It is well known that a planar central configuration of the n-body problem gives rise to solutions
where each particle moves on a specific Keplerian orbit while each particle follows a homographic motion.
Following Meyer and Schmidt [27], we call these solutions as elliptic relative equilibria
(ERE for short).
Specially when e=0, the Keplerian elliptic
motion becomes circular and then all the bodies move around the center of masses along circular
orbits with the same frequency, which are called relative equilibria in literature.
In the three-body case, the linearly stability of any ERE was clearly studied recently (c.f.[6] and [38]).
In fact, the stability of ERE depends on the eccentricity e and a mass parameter β.
For the elliptic Lagrangian solution, the mass parameter is given by βL∈[0,9] by
[TABLE]
For the elliptic Euler solution, the mass parameter is given by βE∈[0,7) in [38].
In [6] and [38],
the authors used Maslov-type index and operator theory
to study the linear stability,
and obtained a full description of the bifurcation diagram.
For the near-collision Euler solutions of 3-body problem,
the linear stability was studied by Hu and Ou in [8].
To our knowledge,
for the general masses of n bodies,
the elliptic Euler-Moulton solutions is the only case
which has been well studied in [39].
The linear stability
of the elliptic Euler-Moulton solutions depends on (n−1) parameters,
namely the eccentricity e∈[0,1) and the n−2 mass parameters
β1,β2,…,βn−2 which defined by (1.14) in [39].
For some special cases of n-body problems,
the linear stability of ERE, which is raised from
an n-gon or (1+n)-gon central configurations with n equal masses,
was studied by Hu, Long and Ou in [5] recently.
For the elliptic relative equilibria of
a general non-collinear central configurations,
even for n=4, the stability problem is quite open.
In [16], the first author studied the linear stability of the planar four body problem when the central configuration is a rhombus. It turns out that it is linearly unstable for all possible masses and all eccentricity.
In [40], the second author studied the linear stability
of ERE of planar 4-body problem with two zero masses.
The most interesting case is when the two small masses tend to the same Lagrangian point L4 (or L5).
There are two cases: the ERE raised from the non-convex central configurations are always linearly unstable;
while for the ERE raised from the convex central configurations,
the linear stability are depends on the parameters.
In this paper, we consider the linear stability of ERE
of the planar restricted 4-body problems.
There are four point masses on the plane, one of which possesses zero mass.
This problems are also referred as the (3+1)-body problems.
The zero mass body is supposed to have no gravitational effect
on three primaries.
As a consequence, the central configuration equations of the restricted 4-body problem can be decomposed to two parts,
one part is the equations of the three-body,
and the other is the action of the three primaries on the zero mass body.
The solution of the first part corresponds to the well-known Lagrange equilateral triangular configurations
and the Euler collinear configurations.
Both configurations exist for all values of the masses.
We will consider the central configurations with the three primaries forming an equilateral
triangle (see Figure 1.1).
In [15], Leandro studied the central configurations of the restricted 4-body problems.
Following his notations,
three primaries m1, m2, and m3 form a standard equilateral triangle and
ris are the distance from mi to m4 respectively.
Three types of possible regions for m4 were found:
the exterior of the triangle and convex configurations region, the exterior of the triangle and non-convex configurations region, and the interior of the triangle region ΠI
(see Figure 1.2).
Note that the exterior regions of the triangle are symmetrical by rotations of 32π about the center of the triangle. Therefore, we restrict our study in following regions (shown in the Figure 1.2).
[TABLE]
where xks are given by (3.7) of [15] and F is given by (3.2) of [15].
By Proposition 4.2 and Corollary 4.3 of [15],
the author proved that there exists only one convex central configuration
which m4 locates in ΠC and only one non-convex central configuration
if m4 locates in ΠN respectively for all positive m1,m2 and m3.
For the linearized Hamiltonian system at the ERE,
we have the following reduction:
Theorem 1.1**.**
For the planar 4-body problem with given masses m=(m1,m2,m3,m4)∈(R+)4, denote the
ERE with eccentricity e∈[0,1) for m by qm,e(t)=(q1(t),q2(t),q3(t),q4(t)). Then
in the limiting case when m4 tends to [math],
the linearized Hamiltonian system at qm,e is reduced to the summation of 3 independent
Hamiltonian systems, the first one is the linearized system of the Kepler 2-body problems at the corresponding Kepler orbit,
the second one is the linearized Hamiltonian system of 3-body problems at the Lagrangian ERE with eccentricity e and the mass parameter βL of (1.5),
and the third one is the essential part ξ
of the linearized Hamiltonian system
given by
[TABLE]
where t∈[0,2π], λ3=1+α+3β and λ4=1+α−3β with
[TABLE]
and for 1≤i≤3, qi,0 and z∗ are the limit positions of mi and m4 respectively when m4 tends to zero.
Remark 1.2**.**
According to the discussion in Section 2, the parameters λ3 and λ4 only depend on
m1, m2
since ∑i=13mi=1.
But the physical meaning of λ3 and λ4
are not straightforward.
Noting that the linear stability of the Keplerian and Lagrangian parts have been studied in [6] and [10],
we only need to study the linear stability of the essential part in this paper.
When m4 locates in ΠN, we have following result.
Theorem 1.3**.**
(i)
If limit position z∗ of the zero mass m4 locates in ΠN
such that q1,0, q2,0, q3,0 and z∗ form a central configuration,
the essential part of the system is linearly unstable.
2. (ii)
If m1=m2=m4=0, then z∗=21+−1(1+23)∈∂ΠN,
the essential part of the system is spectrally stable but linearly unstable.
Denote by Sp(2n) the symplectic group of real 2n×2n matrices.
Following [18] and [20], for any ω∈U={z∈C∣∣z∣=1}, define a real function
Dω(M)=(−1)n−1ωndet(M−ωI2n) for any M in the symplectic group Sp(2n).
Then we can define Sp(2n)ω0={M∈Sp(2n)∣Dω(M)=0} and
Sp(2n)ω∗=Sp(2n)∖Sp(2n)ω0. The orientation of Sp(2n)ω0 at any of its point
M is defined to be the positive direction dtdMetJ∣t=0 of the path MetJ with t>0 small
enough. Let νω(M)=dimCkerC(M−ωI2n). Let
P2π(2n)={γ∈C([0,2π],Sp(2n))∣γ(0)=I} and
γ0(t)=diag(2−2πt,(2−2πt)−1) for 0≤t≤2π.
Given any two 2mk×2mk matrices of square block form
Mk=(AkCkBkDk) with k=1,2,
the symplectic sum of M1 and M2 is defined (cf. [18] and [20]) by
the following 2(m1+m2)×2(m1+m2) matrix M1⋄M2:
[TABLE]
For any two paths ξj∈Pτ(2nj)
with j=0 and 1, let ξ0⋄ξ1(t)=ξ0(t)⋄ξ1(t) for all t∈[0,τ].
As in [20], for λ∈R∖{0}, a∈R, θ∈(0,π)∪(π,2π),
b=(b1b3b2b4) with bi∈R for i=1,…,4, and cj∈R
for j=1,2, some normal forms are given by
[TABLE]
Here N2(e−1θ,b) is trivial if (b2−b3)sinθ>0, or non-trivial
if (b2−b3)sinθ<0, in the sense of Definition 1.8.11 on p.41 of [20]. Note that
by Theorem 1.5.1 on pp.24-25 and (1.4.7)-(1.4.8) on p.18 of [20], when λ=−1 there hold
c2=0 if and only if dimker(M2(−1,c)+I)=1 and
c2=0 if and only if dimker(M2(−1,c)+I)=2.
For more details, readers may refer Section 1.4-1.8 of [20].
For any ξ∈P2π(2n) we define νω(γ)=νω(ξ(2π)) and
[TABLE]
i.e., the usual homotopy intersection number, and the orientation of the joint path ξ∗ξn is
its positive time direction under homotopy with fixed end points, where the path ξn(t)=(2−τt00(2−τt)−1). When ξ(2π)∈Sp(2n)ω0, the index iω(ξ) follows [20]. The pair
(iω(ξ),νω(ξ))∈Z×{0,1,…,2n} is called the index function of ξ
at ω. When νω(ξ)=0 or νω(ξ)>0, the path ξ is called ω-non-degenerate
or ω-degenerate respectively.
For more details readers may refer to [20].
When e=0, the region of (α,β,e) is divided to Ri for 1≤i≤4 (see I, II, III and IV of Section 3) and the sub-regions of R2 and R3 are defined by (3.25 -3.31) when e=0. Then we have following results on ω-Maslov index.
Theorem 1.4**.**
When α≥β>0, the essential part ξα,β,e of the fundamental solutions of the linearized Hamiltonian system by (1.9) satisfies following results on the ω-Maslov-type index and the nullity:
(i)
when e=0, the 1-index and nullity of ξα,β,0 satisfy that
[TABLE]
2. (ii)
when e=0, the −1-index and nullity of ξα,β,0 satisfy that
[TABLE]
3. (iii)
when α≥3β>0, e∈[0,1) and ω∈U, the ω-index and nullity of ξα,β,e satisfy
[TABLE]
Therefore, ξα,β,e(2π) is hyperbolic and linearly unstable;
4. (iv)
when α>β, α>3β−1 and e∈[0,1), the 1-index and nullity of ξα,β,e satisfy
[TABLE]
and when 0<β≤α<3β−1 and e∈[0,1),
i1(ξα,β,e) is positive and odd;
5. (v)
for fixed e∈[0,1) and ω∈U, if we fixed β0∈(0,∞),
iω(ξα,β0,e) is non-increasing in α∈(0,∞);
if we fixed α0∈(0,∞),
iω(ξα,β0,e) is non-decreasing in β∈(0,α0); and iω(ξα,β0,e) tends to infinity when 3β−α→∞.
Since by (i) and (ii) of Theorem 1.4, we have the ±1-index and nullity when e=0.
When m4 locates on ΠC or ΠI, for convenience of the discussion,
two new parameters α~,β~ are introduced by
[TABLE]
Then α~,β~ are two functions of m1,m2 by (1.10) and (1.18).
By (iii) of Theorem 1.4,
we only need to consider the region of α~≥0, β~≥−1 and e∈[0,1).
We further divide this region to RNH and REH by
[TABLE]
In RNH, by (v) of Theorem 1.4,
ν1(ξα,β,e)=0 and there exist two −1-degeneracy surfaces Bs∗ and Bm∗ and the envelope of the ω-degenerate surface Bk.
By these surfaces, RNH is divided into Bs, Bm, Bk and Bh which are defined by (6.33 - 6.39).
For (α~,β~,e)∈RNH, the norm form and the linear stability are given in Theorem 1.5 and Theorem 1.6.
Theorem 1.5**.**
The region RNH is divided into sub-regions Bs, Bm, Bk and Bh where Bh is the hyperbolic regions. When (α~,β~,e)∈Bs∪Bm∪Bk,
the normal form and linear stability of ξ~α~,β~,e(2π)
satisfy following results.
(i)
if (α~,β~,e)∈Bm, ξ~α~,β~,e(2π)≈R(θ1)⋄R(θ2) for some θ1 and θ2∈(π,2π). Thus it is strongly linear stable;
2. (ii)
if (α~,β~,e)∈Bs, ξα,β,e(2π)≈D(λ)⋄R(θ) for some 0>λ=−1 and θ∈(π,2π). Thus and it is elliptic–hyperbolic, and thus linearly unstable;
3. (iii)
if (α~,β~,e)∈Bk. ξα,β,e(2π)≈R(θ1)⋄R(θ2) for some θ1∈(0,π) and θ2∈(π,2π) with 2π−θ2<θ1. Thus it is strongly linearly stable;
Theorem 1.6**.**
When (α~,β~,e)∈Bs∗, Bm∗ or Bk∗, the normal form and the linear stability of ξ~α~,β~,e(2π) satisfy followings.
(i)
If β~s(α~,e)<β~m(α~,e), we have ξ~α~,β~m(α,e),e(2π)≈N1(−1,−1)⋄R(θ) for some θ∈(π,2π). Thus it is spectrally stable and linearly unstable;
2. (ii)
if β~k(α~,e)<β~s(α~,e)=βm(α,e), we have ξ~α~,β~s(α~,e),e(2π)≈−I2⋄R(θ) for some θ∈(π,2π). Thus it is linearly stable, but not strongly linearly stable;
3. (iii)
if β~k(α~,e)<β~s(α~,e)<β~m(α~,e), we have ξ~α~,β~s(α~,e),e(2π)≈N1(−1,−1)⋄R(θ) for some θ∈(π,2π). Thus it is spectrally stable and linearly unstable;
4. (iv)
if β~k(α~,e)<β~s(α~,e)≤β~m(α~,e), we have ξ~α~,β~k(α,e),e(2π)≈N2(e−1θ,b) for some θ∈(0,π) and b=(b1b3b2b4)
satisfying (b2−b3)sinθ>0,
that is, N2(e−1θ,b) is
trivial in the sense of Definition 1.8.11 in p.41 of **[17]**.
Consequently the matrix ξ~α~,β~k(α~,e),e(2π) is spectrally stable and linearly unstable;
5. (v)
if β~k(α~,e)=β~s(α~,e)≤β~m(α~,e),
we have either ξ~α,β~k(α~,e),e(2π)≈N1(−1,1)⋄D(λ) for some −1<λ<0
and is linearly unstable; or ξ~α~,β~k(α~,e),e(2π)≈M2(−1,c) with c1, c2∈R and c2=0. Thus it is spectrally stable and linearly unstable;
6. (vi)
if β~k(α~,e)=β~s(α~,e)=β~m(α~,e), either ξ~α~,β~k(α~,e),e(2π)≈M2(−1,c)
with c1, c2∈R and c2=0 which possesses basic normal form N1(−1,1)⋄N1(−1,1),
or
ξ~α~,β~k(α~,e),e≈N1(−1,1)⋄N1(−1,1).
Thus ξ~α~,β~k(α~,e),e(2π) is spectrally stable and linearly unstable.
When (α~0,β~0,e)∈REH, we find there exist infinitely many 1-degenerate and −1-degenerate surfaces and these surfaces separate REH into sub-regions.
Theorem 1.7**.**
For the given (α~0,β~0,e)∈REH,
there exist 1-degenerate surface functions (α~,e)→β~i(α~,1,e) and −1-degenerate surface functions (α~,e)→β~i(α~,−1,e) with β~2n(α~,1,e)=β~2n−1(α~,1,e). If 1-degenerate surfaces Γn and −1-degenerate surfaces Σn± are defined by
[TABLE]
then we have that
(i)
Γn* starting from curve R3,n∗ when e=0, Γn is perpendicular to the αβ-plane and for each e∈[0,1),
ν1(ξα~,β~2n(α~,1,e),e)=2.
Furthermore, β~2n(α~,1,e) is the real analytic functions in (α~,e);*
2. (ii)
starting from the line R3,n+21∗ defined in (3.26) for n∈N,
two −1-degenerate surfaces Σn± of ξα,β,e(2π) are perpendicular
to the αβ-plane.
Moreover, for each e∈(0,1),
if β~2n−1(α~,−1,e)=β2n(α~,−1,e) with (α~,β~2n−1(α~,−1,e),e)∈Σn− and (α~,β~2n(α~,−1,e),e)∈Σn+,
the two surfaces satisfy ν1(ξα~,β~2n−1(α~,−1,e),e)=ν1(ξα~,β~2n(α~,−1,e),e)=1;
if β~2n−1(α~,−1,e)=β~2n(α~,−1,e)∈Σn+∩Σn−,
the two surfaces satisfy ν1(ξα~,β~2n−1(α~,−1,e),e)=2.
Furthermore, both β2n−1(−1,e) and
β2n(−1,e) are real piece-wise analytic functions in e∈[0,1);
3. (iii)
the 1-degenerate surfaces and −1-degenerate surfaces can be ordered from left to right by
[TABLE]
Moreover, for n1,n2∈N, Γn1 and Σn2± cannot intersect each other;
if n1=n2, Γn1 and Γn2 cannot intersect each other,
and Σn1± and Σn2± cannot intersect each other.
More precisely, for each fixed α~≥0 and e∈[0,1), we have
[TABLE]
Then the linear stability and the normal form of the ξα,β,e(2π) are obtained when (α~,β~,e)∈REH.
Theorem 1.8**.**
For the given α0,β0,e0∈REH, the linear stability and the normal form ξ~α~0,β~0,e0(2π) satisfy following results: for n∈N0,
(i)
if β~2n(α~0,1,e0)<β~0<β~2n+1(α~0,−1,e0),
then i1(ξ~α~0,β~0,e0(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=0, and
i−1(ξ~α~0,β~0,e0(2π))=2n, ν−1(ξ~α~0,β~0,e0(2π))=0. Therefore,
ξ~α~0,β~0,e0(2π)≈R(θ)⋄D(2) for some θ∈(0,π);
2. (ii)
if β~0=β~2n+1(α~0,−1,e0)=β~2n+2(α~0,−1,e0),
then i1(ξ~α~0,β~0,e0(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=0, and
i−1(ξ~α~0,β~0,e0(2π))=2n, ν−1(ξ~α~0,β~0,e0(2π))=2. Therefore,
ξ~α~0,β~0,e0(2π)≈−I2⋄D(2);
3. (iii)
if β~2n+1(α~0,−1,e0)=β~2n+2(α~0,−1,e0) and β~0=β~2n+1(α~0,−1,e0),
then i1(ξ~α~0,β~0,e0(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=0,
and i−1(ξ~α~0,β~0,e0(2π))=2n, ν−1(ξ~α~0,β~0,e0(2π))=1.
Therefore, ξ~α~0,β~0,e0(2π)≈N1(−1,−1)⋄D(2);
4. (iv)
if β~2n+1(α~0,−1,e0)=β~2n+2(α~0,−1,e0) and β~2n+1(α~0,−1,e0)<β~0<β~2n+2(α0,−1,e0),
then i1(ξ~α0,β~0,e0(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=0,
and i−1(ξ~α~0,β~0,e0(2π))=2n+1, ν−1(ξ~α~0,β~0,e0(2π))=0.
Therefore, ξ~α~0,β~0,e0(2π)≈D(−2)⋄D(2);
5. (v)
if β~2n+1(α~0,−1,e0)=β~2n+2(α~0,−1,e0) and β~0=β~2n+2(α~0,−1,e0),
then i1(ξ~α~0,β~0,e0(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=0, and
i−1(ξ~α~0,β~0,e0(2π))=2n+1,
ν−1(ξ~α~0,β~0,e0(2π))=1.
Therefore, ξ~α~0,β~0,e0(2π)≈N1(−1,1)⋄D(2);
6. (vi)
if β~2n+2(α~0,−1,e0)<β~0<β~2n+1(α~0,1,e0),
then i1(ξ~α~0,β~0,e(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=0, and
i−1(ξ~α~0,β~0,e0(2π))=2n+2, ν−1(ξ~α~0,β~0,e0(2π))=0.
Therefore, ξ~α~0,β~0,e0(2π)≈R(θ)⋄D(2)
for some θ∈(π,2π);
7. (vii)
if β~0=β~2n+1(α~0,1,e0)(=β~2n+2(α~0,1,e0)),
then i1(ξ~α~0,β~0,e0(2π))=2n+1, ν1(ξ~α~0,β~0,e0(2π))=2,
and i−1(ξ~α~0,β~0,e0(2π))=2n+2,
ν−1(ξ~α~0,β~0,e0(2π))=0.
Therefore, ξ~α~0,β~0,e0(2π)≈I2⋄D(2).
This paper is organized as follows.
In Section 2, We reduce the linearized Hamiltonian systems at ERE
for the general 4-body problem,
and for the case m4=0,
we will prove Theorem 1.1.
In Section 3, we analyze the linear stability of circular ERE namely e=0.
In Section 4, we study some general properties of the ω-indices. Then in Section 5, 6 and 7 we will discuss the linear stability in
the hyperbolic region which satisfies α≥3β>0, non-hyperbolic region RNH,
and the elliptic-hyperbolic region REH respectively.
Especially, Theorem 1.3 is proved in Section 7.
In Section 8, we apply the results to the cases of m1=m2 by the assistance of the numerical computation. In this paper, we use N to denote the positive integers and use N0 to denote the non-negative integers.
2 The Symplectic Reduction of the Linearized Hamiltonian Systems
2.1 Preliminaries of ω-Maslov-type indices and ω-Morse indices
For T>0, suppose x is a critical point of the functional
[TABLE]
where L∈C2((R/TZ)×R2n,R) and satisfies the
Legendrian convexity condition Lp,p(t,x,p)>0. It is well known
that x satisfies the corresponding Euler-Lagrangian
equation:
[TABLE]
For such an extremal loop, define
[TABLE]
Note that
[TABLE]
For ω∈U, set
[TABLE]
We define the ω-Morse index ϕω(x) of x to be the dimension of the
largest negative definite subspace of
[TABLE]
where ⟨⋅,⋅⟩ is the inner product in L2. For ω∈U, we
also set
[TABLE]
Then F′′(x) is a self-adjoint operator on L2([0,T],Rn) with domain D(ω,T).
We also define the ω-nullity νω(x) of x by
[TABLE]
Note that we only use n=2 in (2.4) from in this paper.
In general, for a self-adjoint linear operator A on the Hilbert space H,
we set ν(A)=dimker(A) and denote by ϕ(A) its Morse index which is the maximum dimension
of the negative definite subspace of the symmetric form ⟨A⋅,⋅⟩. Note
that the Morse index of A is equal to the total multiplicity of the negative eigenvalues
of A.
On the other hand, x~(t)=(∂L/∂x˙(t),x(t))T is the solution of the
corresponding Hamiltonian system of (2.1)-(2.2), and its fundamental solution
γ(t) is given by
[TABLE]
with
[TABLE]
Lemma 2.1**.**
([20], p.172)
For the ω-Morse index ϕω(x) and nullity νω(x) of the solution x=x(t)
and the ω-Maslov-type index iω(γ) and nullity νω(γ) of the
symplectic path γ corresponding to x, for any ω∈U we have
[TABLE]
A generalization of the above lemma to arbitrary boundary conditions is given in [9].
For more information on these topics, we refer to [20].
To measure the jumps between iω(γ)
and iλ(γ) with λ∈U near ω from two sides of ω in U, the splitting numbers SM±(ω) is defined by followings.
Definition 2.2**.**
([18], [20])
For any M∈Sp(2n) and ω∈U, choosing τ>0 and γ∈Pτ(2n) with γ(τ)=M,
we define
[TABLE]
They are called the splitting numbers of M at ω.
For any ω0=e−1θ0∈U with 0≤θ0<2π,
the eigenvalues of M on U are denote by ωj with 1≤j≤p0 which are
distributed counterclockwise from 1 to ω0 and located strictly between 1 and ω0.
Then we have
[TABLE]
The splitting numbers have following properties.
Lemma 2.3**.**
([20], p.198)
The integer valued splitting number pair (SM+(ω),SM−(ω)) defined for all
(ω,M)∈U×∪n≥1Sp(2n) are uniquely determined by the following axioms:
1∘* (Homotopy invariant) SM±(ω)=SN±(ω) for all N∈Ω0(M).*
2∘* (Symplectic additivity) SM1⋄M2±(ω)=SM1±(ω)+SM2±(ω)
for all Mi∈Sp(2ni) with i=1 and 2.*
3∘* (Vanishing) SM±(ω)=0 if ω∈σ(M).*
4∘* (Normality) (SM+(ω),SM−(ω)) coincides with the ultimate type of
ω for M when M is any basic normal form.*
Moreover, by Lemma 9.1.6 on p.192 of [20] for ω∈C and M∈Sp(2n), we have
[TABLE]
The ultimate type of ω∈U for a symplectic matrix M mentioned in the above lemma
is given in Definition 1.8.12 on pp.41-42 of [20] algebraically with its more properties studied
there.
For the reader’s conveniences, following the List 9.1.12 on pp.198-199 of [20],
the splitting numbers (i.e., the ultimate types) for all basic normal forms are given by:
⟨1⟩(SM+(1),SM−(1))=(1,1) for M=N1(1,b) with b=1 or [math].
⟨2⟩(SM+(1),SM−(1))=(0,0) for M=N1(1,−1).
⟨3⟩(SM+(−1),SM−(−1))=(1,1) for M=N1(−1,b) with b=−1 or [math].
⟨4⟩(SM+(−1),SM−(−1))=(0,0) for M=N1(−1,1).
⟨5⟩(SM+(e−1θ),SM−(e−1θ))=(0,1)
for M=R(θ) with θ∈(0,π)∪(π,2π).
⟨6⟩(SM+(ω),SM−(ω))=(1,1) for M=N2(ω,b)
being non-trivial (cf. Definition 1.8.11 on p.41 of [20]) with
ω=e−1θ∈U\R.
⟨7⟩(SM+(ω),SM−(ω))=(0,0) for M=N2(ω,b)
being trivial (cf. Definition 1.8.11 on p.41 of [20]) with
ω=e−1θ∈U\R.
⟨8⟩(SM+(ω),SM−(ω))=(0,0) for ω∈U and M∈Sp(2n)
satisfying σ(M)∩U=∅.
For any symplectic path γ∈P2π(2n) and m∈N, the m-th iteration γm:[0,τ]⟶Sp(2n) is by
[TABLE]
with γm(t)=γ(t−jτ)γ(τ)j for gτ≤t≤(j+1)τ and j∈{0,1,…,m−1}
The next Bott-type iteration formula is will be used in this paper.
Lemma 2.4** ((See [19, Theorem 9.2.1, p. 199).**
.)]
For any z∈U,
[TABLE]
2.2 Two useful maps
In this subsection, we introduce two useful maps for our later discussion.
We define φ,ψ:C→GL(2,R), z=x+−1y by
[TABLE]
where z=x+−1y with x,y∈R.
Thus both φ and ψ are real linear maps.
Moreover, by direct computations, we have the following properties:
Lemma 2.5**.**
(i) If z∈R, then
[TABLE]
(ii) for any z∈C, we have
[TABLE]
(iii) for any z,w∈C, we have
[TABLE]
Specially, we have
[TABLE]
Remark 2.6**.**
For a complex matrix N=(Nij)m×n, the 2m×2n matrix φ(N) is given by
[TABLE]
2.3 The essential part of the fundamental solution
In [27] (cf. p.275), Meyer and Schmidt gave the essential part of the fundamental solution of the
elliptic Lagrangian orbit. Readers may also refer [21] for details.
Based on their method, we reduce the linearized system of the planar restricted 4-body problem to 3 sub-systems.
Suppose the four particles which form one central configuration are in R2 at a1=(a1x,a1y),a2=(a2x,a2y),a3=(a3x,a3y),a4=(a4x,a4y). By identifying R2 with C, we write ais as
[TABLE]
Without lose of generality, we normalize the four masses by
[TABLE]
fix the center of mass at origion and normalize the positions ais by
[TABLE]
Using the notations in (2.21), (2.23) are equivalent to
Firstly, D has two direct eigenvalues: λ1=μ with v1=(1,1,…,1)T, and λ2=0 with
v2=(za1,za2,za3,za4)T.
Namely, by direct computations, we have
[TABLE]
where the last equality of (2.31) holds by (2.27).
Moreover by (2.22)-(2.23), we have
[TABLE]
Let v2=(za1,za2,za3,za4)T.
Because, a1,a2,a3,a4 form a non-colinear central configuration,
v2 is independent with v2. Moreover, v2 is also independent with v1.
So v2 is another eigenvector of D corresponding to eigenvalue λ3=0.
For v3, suppose
[TABLE]
where k∈R,l∈C are defined by
[TABLE]
If v2TM~v2=∑i=1nmizai2=0, we have that k=1 and l=0, i.e., v3=v2.
Then we have
Based on v1,v2 and v3, the unitary matrix A~ is defined by
[TABLE]
where (b1,b2,b3,b4)=v3T, i.e., bi=kzai+lzai,1≤i≤4.
Then ci=Ai4, where Ai4 is the algebraic cofactor of ci.
On the other hand, the signed area of the triangle formed by ai,aj and ak is given by
[TABLE]
Then c1=4k−1Δ234=−4k−1Δ234.
Note that, for any ω∈C,∣ω∣=1, if ci are replaced by ωci,i=1,2,3,4, A~ is also a unitary matrix.
Thus let
[TABLE]
with ρ=m1m2m3m4.
Abusing the notations, we also write v4 as
[TABLE]
Now v1,v2,v3,v4 form a unitary basis of C4.
Note that v1,v2,v3 are eigenvectors of matrix D, then v4 is also an eigenvector of D with the corresponding eigenvalue
[TABLE]
Moreover, we define β1 and β2 by
[TABLE]
In the following, without causing the confusion, we will use ai to represent zai, 1≤i≤4.
By the definition of (2.34) and (2.40),
Dvk=λkvk, k=3,4, read
[TABLE]
For 1≤i≤4, let
[TABLE]
then we have
[TABLE]
Now as in p.263 of [27], Section 11.2 of [21], we define
[TABLE]
where pi, qi, i=1,2,3,4 and G, Z, W1, W2, g, z, w1, w2 are all column vectors in R2.
We make the symplectic coordinate change
[TABLE]
where the matrix A is constructed as in the proof of Proposition 2.1 in [27].
Concretely, the matrix A∈GL(R8) is given by
[TABLE]
where each Ai is a 2×2 matrix given by
[TABLE]
and φ is given by (2.11).
Moreover, by the definition of vi,1≤i≤4, we obtain
[TABLE]
By (2.6), we have
ATMA=φ(A~)Tφ(M~)φ(A~)=φ(A~TM~A~)=φ(I4)=I8
is fulfilled (cf. (13) in p.263 of [27]).
Under the coordinate change (2.45), kinetic energy of the Hamiltonian function of the four-body problems is given by
[TABLE]
and the potential function is given by
[TABLE]
where Uij(z,w1,w2)=∣dij(z,w1,w2)∣mimj
with
Let θ be the true anomaly.
Then based on symplectic transformation in the proof of Theorem 11.10 (p. 100 of [21]),
the resulting Hamiltonian function of the 4-body problem is given by
We now derived the linearized Hamiltonian system at the elliptic relative equilibria.
Proposition 2.7**.**
Using notations in (2.44), elliptic relative equilibrium solution (P(t),Q(t))T of the system (1.2) with
[TABLE]
in time t with the matrix M is given by (2.26),
is transformed to the new solution (Y(θ),X(θ))T in the variable true anomaly θ
with G=g=0 with respect to the original Hamiltonian function H of (2.3), which is given by
[TABLE]
*Moreover, the linearized Hamiltonian system at the elliptic relative equilibrium
ξ0≡(Y(θ),X(θ))T=
(0,σ,0,0,0,0,σ,0,0,0,0,0)T∈R12
depending on the true anomaly θ with respect to the Hamiltonian function
H of (2.3) is given by*
[TABLE]
with
[TABLE]
and
[TABLE]
where β1=0 and
β2 are given by (2.41),
and β11,β12,β22 are given by
[TABLE]
and H′′ is the Hessian matrix of H with respect to its variable Zˉ,
W1ˉ,Wˉ2, zˉ, w1ˉ,wˉ2.
The corresponding quadratic Hamiltonian function is given by
[TABLE]
Proof.
The proof is similar to those of Proposition 11.11 and Proposition 11.13 of [21].
We only need to compute Hzˉzˉ(θ,ξ0), Hzˉwiˉ(θ,ξ0)
and Hwiˉwjˉ(θ,ξ0) for i,j=1,2.
For simplicity, we omit all the upper bars on the variables of H in (2.3) in this proof.
By (2.3), the derivatives of H with respect with the z and wi is given by
[TABLE]
and second derivatives of H with respect with the z and wi by is given by
[TABLE]
where all the items above are 2×2 matrices.
For Uij defined in (2.48) with 1≤i<j≤4, 1≤l≤2,
we have
[TABLE]
and then
[TABLE]
where Φ(z,w1,w2)=dij(z,w1,w2)dij(z,w1,w2)T.
Let
[TABLE]
where ψ is given by (2.11).
Now evaluating these functions at ξˉ0=(0,σ,0,0,0,0,σ,0,0,0,0,0)T∈R12
with z=(σ,0)T,wi=(0,0)T,1≤i≤2, and summing them up,
we obtain
where the second formula holds because of (2.43) and (2.56).
Similarly, we have
[TABLE]
Moreover, we have
[TABLE]
where the second last equality holds because (2.27), and the last equality holds because of (2.43).
Similarly, we have
[TABLE]
By r(θ)=1+ecosθp, σ4=μp and (2.61)-(2.66), the second derivative of H are given by
[TABLE]
Thus the proof is complete.
∎
2.4 The reduction at ERE of Lagrangian central configuration and one zero mass
We consider the central configurations of restricted 4-body problem where three primaries form an equilateral triangle.
We fix m1,m2∈(0,1) such that m1+m2<1,
and let m3=1−m1−m2−ϵ and m4=ϵ with
0<ϵ<1−m1−m2. Therefore, ∑i=04mi=1.
Let q1=0 and q2=1. When ϵ→0, by our assumption,
q3 must tend to one of the Lagrangian points of m1 and m2.
Without lose of generality, in the complex plane, we suppose such Lagrangian point
[TABLE]
Moreover, the limit positions of the zero mass q4 are discussed in [15],
and we denote it by z∗, namely,
[TABLE]
The center of mass of the four particles is
[TABLE]
For i=1, 2, 3 and 4, re-scaling the distance between each body and the center of mass qi−qc by
In the following, we will use the subscript [math] to denote the limit value of the parameters
when ϵ→0.
We now calculate k and l defined by (2.35) for our case.
We first have
[TABLE]
where the second equality holds by m4=ϵ→0 and the third equality holds by (2.69).
Hence by the definition of k in (2.35), k0 is given by
[TABLE]
where one may verify the last equality holds by expending all the brackets and plug in α0 which is defined by (2.70).
By the definition of l0 in (2.35) and direct computations, we obtain that
[TABLE]
Moreover, by (2.39), we obtain for i, j, k∈{1,2,3},
where m3∗=1−m1−m2, the fifth equality holds by (ai,0−aj,0)6=∣ai,0−aj,0∣6=α06 for 1≤i<j≤3,
the sixth equality
holds by (ai,0−aj,0)2(ai,0−aj,0)2=∣ai,0−aj,0∣4=α04 for 1≤i<j≤3
and tenth equality holds by (2.77) and (2.78). Also, β22,0 is given by
[TABLE]
When m4=ϵ→0,
since β12,0=0 of (2.81),
the linearized Hamiltonian system (2.54)
can be decomposed to three independent Hamiltonian systems where
the first one is the linearized Hamiltonian system of the Kepler two-body problem at Kepler elliptic orbit,
and the other two systems can be written as
[TABLE]
with
[TABLE]
for i=1,2.
Thus the linear stability restricted four-body problem in our case
can be reduced to the linear stability problems of system (2.83) with i=1,2.
Let
[TABLE]
for i=1,2.
Then by β1,0=0 in (2.41) and (2.82), D1 is given by
[TABLE]
and hence the two characteristic roots of D1 are:
[TABLE]
where βL is given by
βL=27α02=27[m1m2+(m1+m2)(1−m1−m2)] in (1.5).
As in the proof of Theorem11.14 of [20],
the system (2.83) for i=1 becomes
[TABLE]
thus this system coincides with the essential part of the linearized Hamiltonian system near the elliptic Lagrangian
relative equilibria of the three-body problem with masses m1,m2 and m3=1−m1−m2 because the zero mass has no effect on the other three masses.
The system (2.83) for i=1 has been studied in detail in [6].
We will focus on the system (2.83) for i=2, which is called the essential part in the rest of this paper. It corresponds to the interactions of the zero mass body and three primaries.
The matrix D2 is given by
[TABLE]
The characteristic polynomial det(D2−λI2) of D2 is
By the transformation introduced by Section 2.4 of [6], the system can be related with operator A(α,β,e), i.e.,
[TABLE]
where R(t)=(costsint−sintcost),
Kβ,e=(1+α+3β001+α−3β)
and
S(t)=(cos2tsin2tsin2tcos2t).
By Lemma 2.1,
we have for any (α,β,e)∈[β,+∞)×[0,+∞)×[0,1) and ω∈U,
the Morse indices ϕω(A(α,β,e)) and nullity
νω(A(α,β,e)) on the domain D(ω,2π) satisfy
[TABLE]
where iω(ξα,β,e) is the ω-Maslov-type index and νω(ξα,β,e)=dimker(ξα,β,e(2π)−ωI4) is the nullity of the sympletic path ξα,β,e(t) for t∈[0,2π] where ξα,β,e(t) is the solution of (2.89).
3 Stability of the Circular Orbits
When e=0 and α≥β>0, the orbit of each body is circle and the linearized system (2.89) is given by
[TABLE]
The corresponding characteristic polynomial det(JB2,0−λI) of JB2,0 is given by
[TABLE]
The four roots of p(λ)=0 are given by
[TABLE]
The four characteristic multipliers of the matrix ξα,β,0(2π) are given by
[TABLE]
According our assumption that α≥β≥0, we have divide the region of (α,β,e)∈[0,∞)×[0,∞)×{0} into four sub-regions Ri for 1≤i≤4 as following. The corresponding figure is shown in Figure 1.3
I
The first region R1≡{(α,β)∣α≥β>0,α>49β2}.
In R1, both η1 and η2 are complex numbers because 9β2−4α<0. It yields that λi,±∈C with non-zero imaginary parts. Then the four characteristic multipliers of the matrix ξα,β,0(2π) satisfy σ(ξα,β,0(2π))⊂C∖U.
II
The second region R2≡{(α,β)∣α≥β>0,α≤49β2,α≥3β−1,α≤1}.
In R2, η1 and η2 satisfy that
[TABLE]
Then we have that λi,±∈−1R for 1≤i≤4 and the four characteristic multipliers of the matrix ξα,β,0(2π) satisfy σ(ξα,β,0(2π))⊂U.
III
The third region R3≡{(α,β)∣α≥β>0,α<3β−1}∪{(α,β)∣α=3β−1,α>1}.
Note that α<3β−1 and α≥β0 yield 9β2>α2+2α+1>4α and β≥21.
In R3, η1 and η2 satisfy that
[TABLE]
Therefore, λ1,±∈R∖{0} and λ2,±∈−1R. Then the four characteristic multipliers of the matrix ξα,β,0(2π) satisfy ρ1,±∈R+ and ρ2,±∈U.
IV
The fourth region R4≡{(α,β)∣α>β>0,α≤49β2,α>3β−1,α>1}.
In R4,
η1 and η2 satisfy that
[TABLE]
Therefore, we have that
λi,±∈R. Then the four characteristic multipliers of the matrix ξα,β,0(2π) satisfy σ(ξα,β,0(2π))⊂R+∖{1}.
Note that the R1 and R4 are hyperbolic regions.
We will discuss the linear stability of the essential part in R2 in Section 3.1 and the linear stability in R3 in Section 3.2.
3.1 Stability in region R2
In R2, by (3.5), η1≤0 and η2≤0.
Then we have that λi,±∈−1R.
The four characteristic multipliers of the matrix ξα,β,0(2π) can be written as
[TABLE]
where θi(α,β) are given by
[TABLE]
To determine the maximum and minimum of
θ1(α,β) and θ2(α,β) in R2, by direct computations, we have
[TABLE]
Note (3.10) holds because 9β2−4α<2 in R2 by direct computations.
Therefore the maximum and minimum of θ1 and θ2 in R2 are attained at the boundary of R2 because
[TABLE]
Therefore, in R2, we have that the θ1∈[0,35]
and θ2∈[0,1] and the eigenvalues of ξα,β,0(2π)
are given by σ(ξα,β,0(2π))={e2π−1θ1,e−2π−1θ1,e2π−1θ2,e−2π−1θ2}. If α=49β2 and α=3β−1, θ1=θ2. Therefore, we have that ξα,β,0(2π)≈R(θ1)⋄R(θ2).
By (3.14) and (3.15), 21 is in both the range of θ1 and θ2. By direct computations, we define the −1-degenerate line R2,21∗ in R2 by
[TABLE]
We further define two sub-regions of R2 by
[TABLE]
When (α,β)∈R2,21∗, −1∈σ(ξα,β,0(2π)).
Furthermore, when β∈[325+97,33],
θ1≡21 and θ2∈[423−97,1/2].
Therefore, σ(ξα,β,0(2π))={−1,−1,e2π−1θ2,e−2π−1θ2}.
When
β∈[33,85],
θ2≡21 and θ1∈[0,1/2],
σ(ξα,β,0(2π))={e2π−1θ1,e−2π−1θ1,−1,−1}.
Especially, when (α,β)=(43,33), θ1=θ2=21.
Then σ(ξ43,33,0(2π))={−1,−1,−1,−1}.
For the boundary of R2,
along the segment {(α,β)∈R2∣α=3β−1}, we have that θ1=0 and θ2>0.
Then σ(ξα,β,0(2π))={1,1,e2π−1θ2,e−2π−1θ2} where θ2∈[0,1].
Especially,
when (α,β)=(21,21)∈∂R2, θ1=0 and θ2=1.
Then σ(ξ1/2,1/2,0(2π))={1,1,1,1}.
When (α,β)=(87,85)∈∂R2, we have θ1=0 and θ2=21.
Then σ(ξ1,2/3,0(2π))={1,1,−1,−1}.
When (α,β)=(1,32)∈∂R2, we have θ1=θ2=0. Then σ(ξ1,2/3,0(2π))={1,1,1,1}.
3.2 Stability in region R3
When (α,β)∈R3, by (3.8), the characteristic multipliers are given by
[TABLE]
where θ is given by
[TABLE]
We compute the derivatives of θ with respect to α and β in R3 and obtain that
[TABLE]
Therefore, the maximum and minimum of θ must be attained at the boundary,
i.e., α=β and α=3β−1, or (α,β)=(∞,∞).
By direct computations, along the line α=β, θ tends to infinity when β and α tend to infinity.
Furthermore, when α=3β−1 and β≥32, we have θ≡0.
Then range of θ in R3 is [0,∞).
For (α,β)∈R3 and θ≥0, we use αθ and βθ to denote the values of (α,β) such that
[TABLE]
and hence
[TABLE]
Then define the subsets R3,n∗ and R3,n+21∗ of R3 by setting θ=n and θ=n+21 in αθ(β).
[TABLE]
Note that R3,0∗∩R3,21∗=(87,85) and (21,21)∈R3,0∗∩R3,1∗.
The regions between R3,n∗ and R3,n+21∗ for n∈N0 are defined by
[TABLE]
By (3.23) and direct computations, for given (α,β)∈R3, θ(α,β) is the function of (α,β). Then for the given positive θ1=θ2, αθ1(β) cannot intersect with αθ2(β). Then R3,n+ and R3,n− are pairwise disjoint for all n∈N0.
Note that λ1∈R+∖{1}. Then eigenvalues of ξα,β,0(2π) for (α,β)∈R3 can be given as followings.
(i)
When (α,β)∈R3,0∗, the case of β∈(21,32) has been discussed in Section 3.1.
For β>32, we always have that θ=0
and σ(ξα,β,0(2π))={1,1,e2πλ1,e−2πλ1}.
2. (ii)
Let i∈N0. When (α,β)∈R3,i∗, it yields θ(α,β)=i.
Then ρ2,±=e±2π−1=1σ(ξα,β,0(2π))={1,1,e2πλ1,e−2πλ1}.
3. (iii)
Let i∈N0. When (α,β)∈R3,i+, θ(α,β)∈(i,i+21).
Therefore ρ2,+(α,β)=e2π−1θ(α,β) on upper semi-unit circle in the complex plane C.
Correspondingly ρ2,−(α,β)=e−2π−1θ(α,β) on lower semi-unit circle in C.
Then σ(ξα,β,0(2π))={e2πλ1,e−2πλ1,e2π−1θ(α,β),e−2π−1θ(α,β)} with θ∈(0,π).
4. (iv)
Let i∈N0.
When (α,β)∈R3,i+21∗, it yields θ(α,β)=i+21.
Then ρ2,±=e±−1π=−1 and σ(ξα,β,0(2π))={−1,−1,e2πλ1,e−2πλ1}.
5. (v)
Let i∈N.
When (α,β)∈R3,i−, the angle θ(β)∈(i−21,i).
Thus ρ2,+(α,β)=e2π−1θ(α,β) on the lower semi-unit circle in C.
Correspondingly, ρ2,−(α,β)=e−2π−1θ(α,β) on the upper semi-unit circle in C.
Then σ(ξα,β,0(2π))={e2π−1θ(α,β),e−2π−1θ(α,β)e2πλ1,e−2πλ1} with θ∈(π,2π).
3.3 ±1-indices when e=0
First define an orthogonal basis {f0,1,f0,2,fn,1,fn,2,fn,3,fn,4∣n∈N} of D(1,2π) in (2.3) by
[TABLE]
and for n∈N
[TABLE]
By (2.90) and dtdR(t)=JR(t), A(α,β,0)fn,1 is given by
[TABLE]
Similarly, for n∈N0, it yields that
[TABLE]
where Bn and Bˉn are given by
[TABLE]
The characteristic polynomials of Bn and Bˉn receptively are denoted by pn(λ) and pˉn(λ) which are
[TABLE]
Let i∈N. Fixing α(β)=−i2−1+9β2+4i2,
pn(0)=pˉn(0)=0 if and only if n=i.
Note that when α>3β−1, i.e., (α,β)∈R1∪R2∪R4, (n2+1+α)2−9β2−4n2>0 for all n≥0.
Therefore, when (α,β)∈R1∪R2∪R4, (n2+1+α)2−9β2−4n2>0 and then
[TABLE]
We define that G(n)=n2−9β2+4n2 for given β>1/2 and n≥1. Note that ∂n∂G=2n−9β2+4n24n>0 because 9β2+4n2>25. Therefore, if n1<n2, we have that G(n1)<G(n2), i.e.,
[TABLE]
This yields that pn(0)=pˉn(0)<0 if n<i , and pn(0)=pˉn(0)>0 if n>i . Thus both Bi
and Bˉi have one zero and one positive eigenvalues when n=i; both Bi
and Bˉi with n<i have one
negative and one positive eigenvalues; both Bi
and Bˉi with n>i have two positive
eigenvalues.
Notice that B0 has two positive eigenvalues when α>3β+1; B0 has one positive and one zero eigenvalue when α=3β+1; B0 has one positive and one negative eigenvalue when α<3β+1.
Therefore we have i1(ξα,β,0)=2i+1 and ν1(ξα,β,0)=2 when (α,β)∈R3,i∗.
For (α,β)=(21,21), B0, B1 and Bˉ1 all possess one dimensional degenerate space and one dimension positive definite eigenspace.
When (α,β)∈R3,i+∪R3,i+21∗∪R3,i+1− and i∈N0, then pn(0)=pˉn(0)=0. Similarly to the above argument, we have pn(0)=pˉn(0)<0 if n≤i, and pn(0)=pˉn(0)>0 if n>i .
Thus both Bn and Bˉn with n≤i have a negative and a positive eigenvalues; both Bn and Bˉn with n>i have two positive eigenvalues. Notice that B0 has a negative and a positive eigenvalues, we have i1(ξα,β,0)=2i+1 and ν1(ξα,β,0)=0 for (α,β)∈R3,i+∪R3,i+21∗∪R3,i+1−.
Therefore, we have (1.12) and (1.13) hold for α≥β>0 and n∈N0.
Following the same procedure, to compute i−1(ξα,β,0), we define fˉn,i by
[TABLE]
for n∈N0.
Then we have that
[TABLE]
By arguments similar as the 1-index, we compute the
eigenvalues of A(α,β,0) in the domain D(−1,2π), then the −1-indices of ξα,β,0 and the nullity of ξα,β,0(2π).
Especially when (α,β)∈R2,21⋃(∪n=0∞R3,n+21∗), A(α,β,0) has eigenvalue −1 with geometric multiplicity 2. Thus
[TABLE]
When (α,β)∈R1∪R2∪R4, as the discussion about the 1-index we have that
[TABLE]
When (α,β)∈R3, ξα,β,0(2π) possesses one pair of positive hyperbolic characteristic multipliers
ρ1,±(β) and one pair of elliptic characteristic multipliers ρ2,±(β) on the unit circle. Then
[TABLE]
for some matrix M(2π)∈Sp(2). Due to the nullity of M(2π) is even, M(2π) must be the normal form N1(±1,b) with b=0. Then we have for n∈N
[TABLE]
Note that there exists a path M(t)∈P2π(2) which connecting M(0)=I2 to M(2π) such that the path ξα,β,0(2π) is homotopic to the path D(etα1(β))⋄M(t) for t∈[0,2π].
By the properties of splitting numbers (2.7), for (α,β)∈R3,n+ and ω=−1, we have that
[TABLE]
When (α,β)∈R3,n+1−, we have that
[TABLE]
If M(2π)=R(−2πθ(β)) for (α,β)∈R3,n+,
we have that i−1(ξα,β,0)=2n+2. By (3.46) and the non-decreasing of i−1(ξα,β,0) with respect to β, we must have i−1(ξα,β^++n+1/2+ϵ,0)=i−1(ξα,β^+n+1/2,0)+ν−1(ξα,β^+n+1/2,0)≥2n+4
which contradicts (3.52). Similarly, we cannot have M(2π)=R(−2πθ(β)) when (α,β)∈R3,n+1−. Thus, we must have that M(2π)=R(2πθ(β)) when (α,β)∈R3,0+⋃(∪n=1∞R3,n−∪R3,n+).
Therefore, we have that for α≥β>0 and e=0, the i−1(ξα,β,0) and ν−1(ξα,β,0) are given by (1.14) and (1.15).
4 The ω-Index Properties
In this section, we first discuss the special case β=0 of the index and then the general properties of index.
At first, we consider the case of α=β=0. By (2.90), A(0,0,e) is given by
[TABLE]
The operator A(0,0,e) has been discussed in Lemma 4.1 of [38]. We paraphrase their results in our notations. For details, readers may refer to [38] for details.
Lemma 4.1**.**
For α=β=0 and 0≤e<1, there holds
(i) A(0,0,e) are non-negative definite for the ω=1 boundary condition and
[TABLE]
(ii) A(0,0,e) are positive definite for the ω=1 boundary condition.
Since that 1+α>1 for α>β=0, by Proposition 2 of [7], we have Proposition 4.2.
Proposition 4.2**.**
For α>β=0, the operator A(α,0,e) is positive definite for any ω boundary conditions.
When α,β>0, the operator A(α,β,e) can be written as
[TABLE]
where Aˉ(α,β,e)=βA(α,0,e)+1+ecost3S(t).
Note that for α,β>0 and e∈(0,1), we have that
[TABLE]
We here follow the proof of Proposition 3.5 of [5] and obtain following monotonic of the index and nullity of A(α,β,e).
Lemma 4.3**.**
(i) The ω-Maslov index ϕω(A(α,β,e)) and the corresponding index iω(ξα,β,e) are non-increasing in α∈(0,∞) and they are non-decreasing in β∈(0,∞).
(ii) The sum of ω-Maslov index and nullity ϕω(A(α,β,e))+νω(A(α,β,e)) and the corresponding iω(ξα,β,e)+νω(ξα,β,e) are non-increasing in α∈(0,∞) and are non-decreasing in β∈(0,∞).
Proof.
Note that for given β0>0 and e0∈[0,1), we have that in D(2π,ω) for α2>α1≥0, e0∈[0,1) and any ω∈U,
[TABLE]
Therefore, we have that the operator is increasing respect to α∈(0,∞).
When β2>β1≥0, since A(α,0,e)≥0, then
[TABLE]
where the equality holds only if α=0 and ω=1, i.e., on D(1,2π). Then we have (i) holds.
By the monotonic of the operator A(α,β,e) and Aˉ(α,β,e) in (4.5) and (4.6), we have that (ii) holds. Readers may also refer the proofs of Lemma 4.4 and Corollary 4.5 in [6] to obtain (ii) holds
∎
When α>β=0 and e∈[0,1), we have that the operator A(α,0,e) is given by
[TABLE]
Corollary 4.4**.**
For α≥β>0 and e∈[0,1), if 3β−α>1+2Cn, we have
[TABLE]
where Cn is a constant depending only on n.
Then as 3β−α increases to infinity, the index increases to infinity.
Proof.
We firstly define a space
[TABLE]
Then we have dimEn=n. Let η be a nonzero C∞ function such that
η(m)(0)=η(m)(2π)=0 for any integer m≥0. Then we have
ηEn⊆D(ω,2π) for any ω∈U.
For e∈[0,1), 0=y(t)=R(t)(0,x(t))T∈En, we have
[TABLE]
where we have used the property η(t)x(t)∣t=0=0,
and Cn is a constant which depend on space En because of the finite dimension of En.
When β>31(1+α+(1+e)Cn), we obtain that A(α,β,e) is negative definite on the subspace ηEn of D(ω,2π). Hence
[TABLE]
Therefore, for any given n0∈N, if α≥β>0 such that 3β−α>1+2Cn, then iω(ξα,β,e)≥n0. Then this corollary holds.
∎
5 Stability in the Hyperbolic Region
In this section, we will prove that the operator A(α,β,e) is positive definite with zero nullity when α≥3β>0 and e∈[0,1).
Theorem 5.1**.**
For any ω boundary condition, A(α,β,e) is positive definite for any e∈[0,1) when α≥3β>0. Furthermore, for any α≥3β>0, e∈[0,1) and ω∈U,
[TABLE]
Then ξα,β,e(2π) possesses two pairs of hyperbolic eigenvalues and it is linearly unstable.
Proof.
The operator A(α,β,e) can be written as
[TABLE]
where S(t) is given by (2.90).
When α=3β, the operator A(α,β,e) can be given by
[TABLE]
By the Lemma 5.3, the operator A(0,0,e) is non-negative definite on D(1,2π) with the kernel
[TABLE]
and it is positive definite on D(ω,2π) where ω∈U∖{1}.
The operator 1+ecost6βR(t)(1000)R(t)T is also non-negative definite on D(ω,2π) for ω∈U.
Therefore, we only need to verify that A(3β,β,e) is positive definite on kerA(0,0,e) for any e∈[0,1).
Let c1 and c2 are complex numbers and
[TABLE]
Therefore, we have that ⟨A(3β,β,e)x0,x0⟩>0 for any ω boundary condition by
[TABLE]
where the second inequality holds because 6β(1+ecost)>0 for all β>0 and e∈[0,1).
Additionally, by (i) of Lemma 4.3, when α>3β>0 and e∈[0,1) , the operator A(α,β,e) is positive definite for any ω boundary condition. By (2.91), this proposition holds.
∎
6 Study in the Non-Hyperbolic Region
Note that T given by (1.18) is invertible whose invert is denoted by T−1. The corresponding fundamental solution is defined by ξα,β,e(t)=ξ~α~,β~,e(t) and the corresponding operator A~(α~,β~,e)=A(α,β,e) is given
by
[TABLE]
We divide (α~,β~,e)∈[0,1)×[−1,∞)×[0,1) into two regions RNH and REH by
[TABLE]
By the affine transformation T, we have the direct results from Lemma 4.3 of the index and nullity of the operator A~(α~,β~,e).
Lemma 6.1**.**
(i) The ω-Maslov index ϕω(A~(α~,β~,e)) and the corresponding index iω(ξ~α~,β~,e) are non-increasing in α~∈(0,∞) and they are non-decreasing in β~∈(−1,∞).
(ii) The sum of ω-Maslov index and nullity ϕ~ω(A~(α~,β~,e))+νω(A~(α~,β~,e)) and the corresponding iω(ξ~α~,β~,e)+νω(ξ~α~,β~,e) are non-increasing in α~∈(0,∞) and they are non-decreasing in β~∈(−1,∞).
6.1 The index in RNH
In this part, the 1-index and nullity of A~(α,β,e) will be discussed when (α~,β~,e)∈RNH.
Note that the stability of β~≤−1 has been discussed in Section 5.
Proposition 6.2**.**
For any α~≥0, −1<β~≤0, and e∈[0,1),
the 1-index and nullity satisfy
[TABLE]
Proof.
We prove this proposition in 4 steps.
Step 1.The 1-index and nullity in {(α~,β~,e)∣α~=0,−1<β~≤0,e∈[0,1)}.
If α~=0 and −1<β~≤0, the operator A~(0,β~,e) can be written as
[TABLE]
When β~=−1, for any ω∈U, A~(0,−1,e)=A(0,0,e), the ω-index and nullity is given by
By Lemma 6.1, for −1<β~<0, the ω-index of A~(0,β~,e) is non-decreasing with respect with β~. Then for β~∈(−1,0), the 1-index and nullity of A~(0,β~,e) are given by
[TABLE]
Step 2.The 1-index and nullity in {(α~,β~,0)∣α~>0,β~=0}.
When β=0, e=0 and 0≤α~≤31, the operator A~(α~,0,0) is given by
[TABLE]
By the discussion in the Section 3.1, if β~=0 and 0≤α~<31 i.e., α=3β−1 and 21≤β<32,
the 1-indices and nullity satisfy
[TABLE]
When α~>31, β~=0 and e=0, following the discussion in Section 3.2, we have
[TABLE]
Step 3.The 1-index and nullity in {(α~,β~,e)∣β~=0,α~>0,e∈[0,1)}.
Note that for any e0∈[0,1) and α~≥1,
[TABLE]
where the second inequality and the forth hold because I2+S(t)≥0 for D(ω,2π) and 2(1+ecost)3(1+α~)≥2(1+e0)3(1+α~) when e0∈[0,1) and α~>1.
When α~>1, it yields that 1+e0α~−e0>0. By (6.7), we have
Suppose that x0=R(t)(0,c0)T∈D(1,2π) where R(t) is given by (2.90) and c∈C is a constant.
By direct computations, we have A~(α~,0,e)x0=0 for α~≥0.
This yields ν1(A~(α~,0,e))≥1.
Together with (6.15), for α~≥0,
[TABLE]
Above all, for all e∈[0,1), the 1-index and nullity satisfy
[TABLE]
**Step 4.**The 1-index and nullity in {(α~,β~,e)∣α~>0,−1<β~<0,e∈[0,1)}.
By (ii) of Lemma 6.1 and (6.21), the 1-index and nullity satisfy
[TABLE]
By Theorem 7.3, the nullity must be even if β~=0. Therefore, when α~>0, −1<β~<0 and e∈[0,1),
[TABLE]
Then we have this proposition holds.
∎
Proposition 6.3**.**
For (α~,β~,e) where α~≥0, −1<β~≤0 and e∈[0,1), ω-index and nullity satisfy
[TABLE]
Especially, for given e0∈[0,1), when α~>41+45e0 and −1<β~≤0,
[TABLE]
Proof.
By the discussion in the Section 3.1, for β~=0 and 0≤α~<31, i.e., α=3β−1 and 21≤β<32,
and in the Section 3.2 for α~>31,
[TABLE]
By (6.12) and (6.26), when 1+e0α~−e0>41, i.e., α~>41+45e0, following similar arguments, we have
By (6.7) and (i) of Lemma 6.1, we also have that for α~∈(0,2),
[TABLE]
and
[TABLE]
Again by Lemma 6.1, (6.24) holds.
Then we have this proposition holds
∎
By the discussion in Theorem 5.1 and Proposition 6.3, especially (6.26), we have that there exist two −1-degenerate surfaces. Then for α~>0, e∈[0,1), we let β~1(α~,e), β~2(α~,e) be the two −1-degenerate surfaces where the −1-index changes and further define β~s(α~,e) and β~m(α~,e) by
[TABLE]
Note that, when e=0, β~1(α~,0)=β~2(α~,0) and (α~,β~1(α~,0))=TR2,21∗ where R2,21∗ is given by (3.16).
When e>0, β~s(α~,e) and β~m(α~,e) bifurcate from R2,21∗.
We define the boundary of the elliptic region in RNH by
[TABLE]
Note that for any given α~0>0, if β~=−1, i.e., α=3β, σ(ξ~α~,β~,e(2π))∩U=∅. Therefore for any (α~,e), β~k(α~,e) is well defined.
By the definition of (6.30) and (6.31), we have that for the given α~0 and e0∈[0,1), if β~s(α0,e0) exists, following holds
[TABLE]
Then we define the −1-degenerate surfaces and the elliptic boundary by
[TABLE]
The regions between them are defined as Bs, Bm, Bk ,and Bh of RNH by
[TABLE]
Proposition 6.4**.**
For (α~,β~,e)∈RNH, the −1-index and nullity of ξ~α~,β~,0 satisfy
[TABLE]
Proof.
When e=0, as the discussion in Section 3.1, the two degenerate surfaces satisfy (α~,β~s)=(α~,β~m)∈TR2,21∗
where R2,21∗ is given by (3.16).
For 0<e<1, by the definition of βs(α,e) and βm(α,e) satisfying for α>0 and e∈[0,1) in (6.30),
we have that −1-index stays the same and only changes when (α,β,e)∈Bm∗∪Bs∗.
Then we have this proposition holds.
∎
Lemma 6.5**.**
(i) For the given α~0 and e0, if
(α~0,β~1,e0) and (α~0,β~2,e0) are both in RNH with −1<β~1≤β~2<0
and ξ~α~0,β~2,e0(2π) is hyperbolic, then ξ~α~0,β~1,e0(2π) is hyperbolic.
Consequently, the hyperbolic region of ξ~α~,β~,e in RNH is connected.
(ii) For (α~,β~,e)∈Bh, every matrix ξ~α~,β~,e(2π) is hyperbolic.
Thus Bk∗ is the boundary set of this hyperbolic region.
(iii) For the any e∈[0,1), and α~∗∈(0,∞),
the total multiplicity of ω degeneracy of
[TABLE]
for t∈[0,1] with α~(t)=tα~∗ and β~(t)=−t satisfies that
Suppose that ξ~α~,β~2,e(2π) is hyperbolic. This implies ϕω(A~(α,β2,e))=0 and νω(A~(α,β2,e))=0. Then ϕω(A~(α,β1,e))=0 and νω(A~(α,β1,e)) for any ω∈U. Therefore ξ~α~,β~,e(2π) must be hyperbolic for all β∈[0,β2).
Note that when β~=−1 and α~>0, the matrix ξ~α~,β~,e is hyperbolic by Theorem 5.1.
Therefore, the hyperbolic region of ξ~α~,β~,e is connected in RNH.
(ii) By the definition of β~k(α~,e), there exists a sequence{β~i}i∈N satisfying β~i<β~k(α,e), β~i→β~k(α~,e), and ξ~α~,β~i,e(2π) is hyperbolic.
Therefore ξ~α~,β~,e(2π) is hyperbolic
for every β~∈[−1,β~k(e)) by (i).
Then (6.31) holds and β~k(α~,e) is the envelope surface of this hyperbolic region.
(iii) Note that both ξ~0,0,e(2π) and ξ~α∗,−1,e(2π) are both non-degenerate when ω∈U∖{1}.
The corresponding operator path is defined by γ∗(t)=A(α~(t),β~(t),e).
For α~∗∈(0,∞) and t0∈(0,1) such that A~(α~(t0),β~(t0),e) is
degenerate, the ω-index must decrease strictly.
By Theorem 5.1 and Lemma 6.1, there exist at most two t1 and t2 such that
at each of which the ω-index decreases
by 1 if t1=t2, or the ω-index decreases by 2 if t1=t2. Suppose that the two values are given by t1=t1(α~∗,e)
and t2=t2(α~∗,e) such that for ϵ>0 small enough, we have that
ϕω(γ∗(0))=ϕω(γ∗(t1−ϵ)), ϕω(γ∗(t1))=ϕω(γ∗(t2−ϵ)) and ϕω(γ∗(t2))=ϕω(γ∗(1)).
Then we have that
[TABLE]
Then we have that (iii) of this lemma holds.
∎
Corollary 6.6**.**
For e∈[0,1) and α~∗∈(0,∞), suppose the continuous path γ(t) is defined by (6.48). There exists t∗∈(0,1) such that γ(t∗)=ξ~α~(t∗),β~(t∗),e(2π)∈Bs∗, and
[TABLE]
Proof.
Fix α~∗ and e∈[0,1). There exists a t∗ such that γ(t∗)∈Bs∗. Then if (t∗α~∗,−t∗,e)∈Bs∗ and (t∗α~∗,−t∗,e)∈/Bm∗,
[TABLE]
if (t∗α~∗,−t∗,e)∈Bs∗∩Bm∗,
[TABLE]
Together with (iii) of Lemma 6.5, we have that (6.53) holds.
∎
Proposition 6.7**.**
The function β~k(α~,e) is continuous in α~ and e.
Proof.
We prove this proposition by contradiction. Suppose that β~k(α~,e) is not continuous in α~ or e. There must exist some (α^,e^) and a sequence {(α~i,ei)}i=1∞⊂[0,∞]×[0,1)∖{(α^,e^)} and β~0∈[−1,0] such that
[TABLE]
We discuss the two cases of the continuity according to the sign of β~0−β~k(α^,e^). By the continuity of the eigenvalues of the matrix ξ~α~,β~,e(2π) and by (6.31) following holds.
[TABLE]
By the definition of β~k(α^,e^) and (i) of Lemma 6.5, we must have β~k(α^,e^)<β0.
Now we suppose β~k(α^,e^)<β~0. By the continuity of β~s(α~,e) and the definition of β~0,
[TABLE]
By the definition of β~k(α^,e^), let ω0∈σ(ξ~α^,β~k(α^,e^),e^(2π))∩U.
Let L={(α^,β~,e^)∣β~∈[−1,β~k(α^,e^))}, V={(α~,−1,e)∣α~∈(0,∞),e∈[0,1)}, and Li={(α~i,β~,ei)∣β~∈[−1,β~k(α~i,ei)]}.
[TABLE]
In particular, we have
[TABLE]
Therefore, by the definition of ω0, there exists β^∈(β~k(α^,e^),β~0) sufficiently close to β~k(α^,e^) such that
[TABLE]
Note that (6.61) holds for all β~∈(β^k(e),β^0]. Also (α^,β^,e^) is an accumulation point of ∪i≥1Li. This yields there exists (α~i,β~i,ei)∈Li such that ξα~i,β~i,ei is ω0-degenerate.
Moreover β~i→β^0 and ξα~i,β~i,ei(2π)→ξα^,β~0,e^(2π) as i→∞.
Then we have following contradiction for i≥1 large enough
[TABLE]
Then we have the continuity of β~k(α~,e) in α~ and e.
∎
(i) By the Bott-type formula (Theorem 9.2.1 in p. 199 of [17]), the index and nullity of 2nd-iteration of the symplectic path ξ~α~,β~,e(t) satisfies
[TABLE]
where ν1(ξ~α~,β~,e)=0 when (α~,β~,e)∈RNH. Therefore, by (6.35) and (6.39), the 2-iteration of the index is given by
[TABLE]
Follow the discussion in the proof of Theorem 1.2 of [10], if (α~,β~,e) satisfies β~=βm(α~,e) and β~=βs(α~,e), the matrix ξ~α~,β~,e(4π)=ξ~α~,β~,e2(2π) is non-degenerate with respect with eigenvalue 1.
For (i), suppose ωi=e−1θi∈σ(ξ~α~,β~,e(2π)∩U), θi∈(0,π). Note that i−1(ξ~α~,β~,e)=2, and by (2.7)
[TABLE]
It yields that
[TABLE]
Then we have that Sξ~α~,β~,e−(ωi)=0, by the list of splitting number in Section 2.
Therefore, there exist the two ω1 and ω2 such that Sξ~α~,β~,e+(ωi)=1.
Then we have (i) of Theorem 1.5 holds.
(ii) Note that i1(ξ~α~,β~,e2)=1 implies that i−1(ξ~α~,β~,e)=1.
Therefore, still by (6.64), there exists exact one eigenvalue ω=e−1θi∈σ(ξ~α~,β~,e(2π)∩U) for θ∈(0,π) with the splitting number (1,0).
By the splitting number the list of splitting number in Section 2, we must have ξ~α~,β~,e(2π)≈D(λ)⋄R(θ).
Also note that i1(ξ~α~,β~,e)=0 implies λ<0.
Then we have (ii) of Theorem 1.5 holds.
(iii)
Suppose that (α~0,β~0,e0)∈Bk.
By (i) and (ii) of Lemma 6.5, the matrix M≡ξ~α~0,β~0,e0(2π) is not hyperbolic with at least one pair of on the unit circle U.
Furthermore, by the definition of β~k(α~0,e0) and β~s(α~0,e0), ±1∈/σ(ξ~α~0,β~0,e0(2π)).
Suppose that
[TABLE]
where λ1∈U\R
and λ2∈(U∪R)\{±1,0}.
If λ2∈R∖{±1,0}, the normal form is given by ξ~α~0,β~0,e0(2π)≈D(λ)⋄R(θ) for some θ∈(0,π)∪(π,2π). Then by (2.7), we obtain following contradiction.
[TABLE]
Then we have λ2∈U∖R and
ξα0,β0,e0(2π)≈R(θ1)⋄R(θ2) for θ1, θ2∈(0,π)∪(π,2π).
Again as (6.67), we have that
[TABLE]
Note that if θ1 and θ2 locate at the same interval (0,π) or (π,2π), the right hand side will be ±2. Thus, we must have that θ1∈(0,π) and θ2∈(π,2π).
Suppose that If θ1=2π−θ2, following equation holds.
[TABLE]
where ω=exp(−1θ1).
This is a contradiction with (iii) of Lemma 6.5.
If 2π−θ2>θ1, for ω=exp(−1θ1), we have that
[TABLE]
where M=ξ~α~0,β~0,e0(2π).
This contradiction yields that 2π−θ2<θ1.
Then we have (ii) of Theorem 1.5 holds.
∎
Lemma 6.8**.**
For some (α~,β~0,e)∈RNH, if ξ~α~,β~0,e(2π)≈M2 where M2 is given by (1.11) with c1, c2∈R
holds,
or it possesses the
basic normal form N1(−1,a)⋄N1(−1,b) and a, b∈R, then ξ~α~,β~,e(2π) is hyperbolic for all β~∈[−1,β~0).
Proof.
Note that the basic normal form of the matrix M2(−1,c) is either N1(−1,a^)⋄N1(−1,b^) or N1(−1,a^)⋄D(λ) for some a^, b^∈R and 0>λ=−1. Thus for any ω∈U∖{1}, by the study in Section 9.1 of
[20], we obtain
[TABLE]
where M=ξ~α~,β~0,e(2π). Then we have that iω(ξ~α~,β~0,e)=0 for all ω∈U. Note that ϕω(A~(α~,β~0,e))=iω(ξ~α~,β~0,e) and νω(A~(α~,β~0,e))=νω(ξ~α~,β~0,e).
Now from ϕω(A~(α~,β~0,e))=0 and the monotonic of eigenvalues of A~(α~,β~0,e) in Lemma 6.5, we have that A~(α~,β~,e)>0 for all β~∈[−1,β~0) on D(ω,2π). Therefore, νω(ξ~α~,β~,e)=νω(A~(α~,β~,e))=0 holds for all β~∈[−1,β~0). Then this lemma holds.
∎
(i) Let e∈[0,1) and α~∈[0,∞) satisfy β~s(α~,e)<β~m(α,e).
Then Corollary 6.6 implies ν−1(ξ~α~,β~m(α~,e),e(2π))=1.
As the limit case of (i) and (ii) of 1.5,
we have the eigenvalues of matrix ξ~α~,β~m(α~,e),e(2π) are all on U and the normal form is either M≈M2(−1,c) for some c2=0 or M≈N1(−1,1)⋄R(θ) for some θ∈(π,2π).
By Lemma 6.8 and β~s(α~,e)<β~m(α~,e), we have that M≈M2(−1,c) for some c2=0 cannot holds.
The normal form is given by M≈N1(−1,1)⋄R(θ).
So M is spectrally stable and linearly unstable.
(ii) Let e∈[0,1) and α~∈[0,∞) satisfy β~k(α~,e)<β~s(α~,e)=β~m(α~,e).
As the limit case of (i) and (ii) of the Theorem 1.6 and Lemma 6.8,
the normal form of the matrix M≡ξ~α~,β~s(α~,e),e(2π) is either M≈N1(−1,a)⋄N1(−1,b) for some a, b∈{−1,1},
or M≈−I2⋄R(θ) for some θ∈(π,2π).
However, the case of M≈N1(−1,a)⋄N1(−1,b) is impossible by Lemma 6.8.
Then we have that M≈−I2⋄R(θ) for some θ∈(π,2π) and it is linear stable but not strongly linear stable.
(iii) Let e∈[0,1) and α~∈[0,∞) satisfy β~k(α~,e)<β~s(α~,e)<β~m(α~,e).
As the limiting case of Cases (ii) and (iii) of Theorem 1.6, the normal form of the matrix M≡ξ~α~,β~s(α~,e),e(2π)
must satisfy either M≈N1(−1,−1)⋄R(θ) for some θ∈(π,2π) or M≈M2(−1,c) for some c2=0.
Here the second case is also impossible by Lemma 6.8, and the conclusion of (iii) follows.
(iv)
Let e∈[0,1) and α~∈[0,∞) satisfy β~k(α~,e)<β~s(α~,e)<β~m(α~,e).
As the limiting case of the cases (iii) of Theorem 1.6,
the matrix ξ~α~,β~k(α~,e),e(2π) must have Krein collision eigenvalues σ(M)={λ1,λˉ1,λ2,λˉ2} with λ1=λˉ2=e−1θ for some θ∈(0,π)∪(π,2π).
By the Proposition 6.2, Proposition 6.3 and the definition of β~k(α~,e),
±1 cannot be the eigenvalue of ξ~α~,β~k(α~,e),e(2π). Therefore, we must have that M≈N2(ω,b) for ω=e−1θ and some matrix
b=(b1b3b2b4)
which has the form of (25-27) by Theorem 1.6.11 in p. 34 of [17].
Because (I2⋄−I2)−1N2(e−1θ,b)(I2⋄−I2)=N2(e−1(2π−θ),b^) where
b^=(b1−b3−b2b4).
We can always suppose θ∈(0,π) without changing the fact M≈N2(ω,b).
Note that by (6.31) and Lemma 6.5, we have iω(ξ~α~,β~k,e)=0.
Suppose b2−b3=0, by Lemma 1.9.2 in p. 43 of [17],
νω(N2(ω,b))=2 and then N2(ω,b) has basic normal form R(θ)⋄R(2π−θ) by the study in case 4
in p. 40 of [17].
Thus we have following contradiction
[TABLE]
Therefore b2−b3=0 must hold. Then we obtain
[TABLE]
By ⟨6⟩ and ⟨7⟩ in the list of splitting number in Section 2, we obtain that N2(ω,b) must be
trivial.
Then by Theorem 1 of [41], the matrix M is spectrally stable and is linearly unstable as claimed.
(v) Let e∈[0,1) and α~∈[0,∞) satisfy β~k(α~,e)=β~s(α~,e)<β~m(α~,e). Note that −1 must be an eigenvalue of M≈ξ~α~,β~k(α~,e),e(2π) with the geometric multiplicity 1 by Proposition 6.4.
As the limit case of (ii) and (iii) of Theorem 1.5, the matrix M must satisfy either M≈M2(−1,b) with b1,
b2∈R and b2=0, and thus is spectrally stable and linearly unstable;
or M≈N−1(−1,a)⋄D(λ) for some a∈{−1,1} and −1=λ<0. Then in the later case we obtain
[TABLE]
Then by ⟨3⟩ and ⟨4⟩ inthe list of splitting number in Section 2, we must have a=1.
Thus M=ξ~α~,β~k(α~,e),e(2π) is hyperbolic (elliptic-hyperbolic) and linearly unstable.
Note that by the above argument, the matrix M2(−1,b) also has the basic
normal form N1(−1,1)⋄D(λ) for some −1=λ<0.
(vi) Let e∈[0,1) and α~∈[0,∞) satisfy β~k(α~,e)=β~s(α~,e)=β~m(α~,e).
As the limiting case of
cases (i), (ii) and (iii) of Theorem 1.5, −1 must be the only eigenvalue of
M=ξ~α~,β~k(α~,e),e with ν−1(M)=2 by Proposition 6.4. Thus the matrix M must satisfy M≈M1(−1,c) with c=0 and v−1(M2(−1,c))=2; or M≈N1(−1,a^)⋄N1(−1,b^) for some a^ and b^∈{−1,1}. In both case M possesses the basic normal form N1(−1,a^)⋄N1(−1,b^) for some a^ and b^∈{−1,1}. Thus we obtain
[TABLE]
Then by ⟨3⟩ and ⟨4⟩ inthe list of splitting number in Section 2, we must have a=b=1 similar
to our above study for (v). Therefore it is spectrally stable and linearly unstable as claimed.
∎
Next, we discuss one boundary of the RNH namely β~=0. When β~=0 and α~=0, the operator A~(0,0,e) is the same as the operator A(βL,e) given by (2.29) of [6] when βL=0.
The we have that for e∈[0,1), the index and nullity satisfy
(6.7).
The norm form of ξ~0,0,e(2π) is given by
[TABLE]
By the continuity of the eigenvalues of ξ~0,0,e(2π) and ν−1(ξ~α~,0,e(2π))=0 when α~≥23 by Proposition 6.3, we must that
α~s(e) is the intersection curve of β~s(α~,e)=0,
α~m(e) is the intersection curve of β~m(α~,e)=0, and α~k(e) is the intersection curve of β~k(α~,e)=0.
Furthermore, α~s(0)=α~m(0)=41 and α~k(0)=31.
Similiar to Proposition 6.4, we have following results and omit the proof.
Proposition 6.9**.**
When β~=0, the −1-index and nullity of ξ~α~,β~,e satisfy
[TABLE]
Following the discussion in the proof of Theorem 1.6, by Proposition 6.9 and Proposition 6.2,
we can have the norm form of ξ~α~,0,e(2π)
when (α~0,β~0,e)∈REH∩RNH, namely, β~=0. The intersection β~∗(α~,e) with β~=0 are denoted by α~∗(e) where ∗=s,m,k respectively.
Theorem 6.10**.**
For e∈[0,1), the normal form and linear stability of ξ~α~,0,e(2π) satisfy followings.
(i)
If α~=0, we have ξ~α~,0,e(2π)≈I2⋄N1(1,1).
Thus it is spectrally stable and linear unstable;
2. (ii)
if 0<α~<α~m(e), we have ξ~α~,0,e(2π)≈R(θ)⋄N1(1,1) with θ∈(π,2π).
Thus it is spectrally stable and linear unstable;
3. (iii)
if α~m(e)<α~s(e), we have ξ~α~m(e),0,e(2π)≈N1(−1,1)⋄N1(1,1) with θ∈(π,2π).
Thus it is spectrally stable and linear unstable;
4. (iv)
if α~m(e)<α~s(e) and α~m(e)<α~<α~s(e),
we have ξ~α~,0,e(2π)≈D(λ)⋄N1(1,1) with 0>λ=−1.
Thus it is spectrally unstable;
5. (v)
if α~m(e)<α~s(e), we have ξ~α~,0,e(2π)≈N1(−1,−1)⋄N1(1,1).
Thus it is spectrally stable and linear unstable;
6. (vi)
if α~m(e)≤α~s(e)<α~k(e) and α~s(e)<α~≤α~k(e), we have ξ~α~,0,e(2π)≈R(θ)⋄N1(1,1) with θ∈(0,π).
Thus it is spectrally stable and linear unstable;
7. (vii)
if α~>α~k(e), we have ξ~α~,0,e(2π)≈D(λ)⋄N1(1,1) with with 0<λ=1.
Thus it is spectrally unstable;
8. (viii)
if α~m(e)=α~s(e)<α~k(e), we have ξ~α~m(e),0,e(2π)≈−I2⋄N1(1,1).
Thus it is spectrally stable and linear unstable;
9. (ix)
if α~m(e)<α~s(e)=α~k(e), we have ξ~α~s(e),0,e(2π)≈N1(−1,−1)⋄N1(1,1).
Thus ξ~α~,β~k(α~,e),e(2π) is spectrally stable and linearly unstable;
10. (x)
if α~m(e)=α~s(e)=α~k(e), ξ~α~k(e),0,e(2π)≈−I2⋄N1(1,1).
Thus ξ~α~,β~k(α~,e),e(2π) is spectrally stable and linearly unstable.
The proof of this theorem is similar as the one of Theorem 1.6. We omit it here.
7 Stability in the Elliptic-Hyperbolic Region
In this section, we will discuss the linear stability in REH.
Firstly, we consider the degenerate surfaces in REH.
7.1 Degenerate surfaces
Since A~(α~,β~,e) is a self-adjoint operator on D(ω,2π),
and a bounded perturbation of the operator −dt2d2I2, A~(α~,β~,e) has discrete spectrum on D(ω,2π).
Thus we can define the n-th degenerate point of β~ for α~≥0, ω∈U and e∈[0,1):
[TABLE]
Furthermore, we define that the degenerate surfaces of ξ~(α~,β~,e)(2π) by
[TABLE]
Additionally, when α~=0 and β~→∞, the iω(ξ~α~,β~,e)+νω(ξ~α~,β~,e) tends to infinity and when α~=β~=0, iω(ξ~0,0,e)+νω(ξ~0,0,e)=2 when ω=1.
Indeed, ξ~α~,β~,e(2π) is ω-degenerate at surface (α~,β~n(α~,ω,e),e) respectively, i.e.,
[TABLE]
Otherwise, if there existed some small enough ϵ>0 such that β~=β~n(α~,ω,e)−ϵ would
satisfy [iω(ξ~α~,β~,e)+νω(ξ~α~,β~,e)]−[iω(ξ~0,0,e)+νω(ξ~0,0,e)]≥n in (7.1),
it would yield a contradiction.
By Lemma 6.1, β~n(α~,ω,e) is non-decreasing with respect to n for fixed α~, ω and e.
For fixed ω,
Πn(ω,e) called the n-th ω-degenerate surface is continuous surface with respect to α~ and e .
Lemma 7.1**.**
For any fixed n∈N and ω∈U, the degenerate surface Πn(ω,e) is continuous with respect to α~ and e.
Proof.
We always assume that n and ω are fixed. In fact, if the function β~n(α~,ω,e) is not continuous in (α~,e),
then there exist some (α~∗,e∗), a sequence {(α~i,ei)∣i∈N}
and α~0≥0 such that
[TABLE]
By (7.3), we have ω∈σ(ξ~α~i,β~n(α~i,ω,ei),ei(2π)).
By the continuity of eigenvalues of ξ~α~,β~,e(2π) with respect to α~ and e, and
(7.4), we have ω∈σ(ξ~α~,β~n,e(2π)),
and hence
[TABLE]
We distinguish two cases according to the sign of the difference β~0−β~n(αˉ,ω,e).
For convenience, let
[TABLE]
If β~0<β~n(α~∗,ω,e∗), firstly we must have g(α~∗,β~0,e∗)<n.
Otherwise by the definition of β~n(α~∗,ω,e∗), we must have β~n(α~∗,ω,e∗)≤β~0.
Let βˉ∈(β0,β~n(α~∗,ω,e∗)) such that νω(ξ~α~∗,βˉ,e∗)=0
for any β~∈(β~0,βˉ]. By the continuity of eigenvalues of ξ~α~,β~,e(2π) with
respect to α~, β~ and e, there exists a neighborhood O of (α~∗,βˉ,e∗)
such that ν(ξ~α~,β~,e)=0 for any (α~,β~,e)∈O. Then iω(ξ~α~,β~,e), and
hence g(α~,β~,e) is constant in O.
By (7.4), for i large enough,
we have β~n(α~i,ω,ei)<βˉ and (α~i,βˉ,ei)∈O, and hence
g(α~i,βˉ,ei)≥g(α~i,β~n(α~i,ω,ei),ei)≥n.
Therefore, we have g(α~∗,βˉ,e∗)≥n.
By the definition of (7.1), we have β~n(α~∗,ω,e∗)≤βˉ
which contradicts βˉ∈(β~0,β~n(α~∗,ω,e∗)).
If β~n(α~∗,ω,e∗)<β~0,
there exists βˉ∈(β~n(α~∗,ω,e∗),β~0) such that νω(ξ~α~∗,β~,e∗)=0
for any β~∈(β~n(α~∗,ω,e∗),βˉ].
By the continuity of eigenvalues of ξ~α~,β~,e(2π) with respect to α~, β~ and e,
there exists a neighborhood U of (α~∗,βˉ,e∗) such that ν(ξ~α~,β~,e)=0
for any (α~,β~,e)∈U.
Then iω(ξ~α~,β~,e), and hence g(α~,β~,e) is constant in U.
By (7.4), for i large enough,
we have βˉ<β~n(α~i,ω,ei) and (α~i,βˉ,ei)∈U.
g(α~i,βˉ,ei)=g(α~,βˉ,e)≥n implies β~n(α~i,ω,ei)≤βˉ, a contradiction.
Thus the continuity of β~n(α~,ω,e) in α~, e is proved.
∎
7.2 The elliptic-hyperbolic region
Note that in Lemma 7.2, we will discuss that the degenerate curves when e=0.
To be consistence with the discussion in Section 3.2, we use the notations (α,β) instead of (α~,β~).
Lemma 7.2**.**
When ω=1 and e=0, the degenerate surfaces satisfy
[TABLE]
Proof.
As in Section 3.2, we have i1(ξ1/2,1/2,0)+ν1(ξ1/2,1/2,0)=3, and if (α,β)∈R3,m+1∗, we have ν1(α,β,0)=2. As (7.6), we define
[TABLE]
and
[TABLE]
For n=2m−1 or 2m, [i1(ξα,β,0)+ν1(ξα,β,0)]−[i1(ξ1/2,1/2,0)+ν1(ξ1/2,1/2,0)]≥n is equivalent to (α,β)∈(∪i≥m+1∞R3,i∗∪R3,i+)⋃(∪i=m+2∞R3,m+2−).
Then the minimal value of β in (α,β)∈(∪i≥m+1∞R3,i∗∪R3,i+)⋃(∪i=m+2∞R3,m+2−) such that A(α,β,e) is degenerate on
D(1,2π) is (α,β)∈R3,m+1∗. Thus applying T−1, we obtain (7.7).
∎
Note that when β~=0, we have already discussed in Proposition 6.2 and the nullity is always odd.
When (α~,β~,e)∈RNH∪REH, we have following theorem.
Theorem 7.3**.**
For any given (α~,β~,e)∈RNH∪REH, every
1-degenerate surface has even geometric multiplicity.
Proof.
The statement has already been proved for e=0 in (1.13).
We will give the proof when e=0.
We notice that the proof will be simple if we use parameters α,β.
Therefore, we consider the region T−1(REH∪RNH)={(α,β,e)∣0<β<α<3β,α=3β−1,e∈[0,1)}.
Once we have the kernel of A(α,β,e)z=0 in D(1,2π) has even dimensions for (α,β,e)∈T−1(RNH∪REH),
we have this theorem holds.
Claim. *If A(α,β,e)z=0
has a solution z∈D(1,2π) for a fixed value e∈(0,1), there exists a second periodic
solution which is independent of z. *
If the claim holds, then the space of solutions of A(α,β,e)z=0 is the direct
sum of two isomorphic subspaces, hence it has even dimension.
This method is originally due to R. Matínez,
A. Samà and C. Simò in [25].
Here we follows the arguments from Theorem 4.8 of [38].
Let z(t)=R(t)(x(t),y(t))T be a nontrivial solution of A(α,β,e)z(t)=0, then it yields
[TABLE]
By Fourier expansion, x(t) and y(t) can be written as
[TABLE]
Then the coefficients must satisfy the following uncoupled sets of recurrences:
[TABLE]
and
[TABLE]
where
[TABLE]
Thus det(B1)=α2+4α−9β2=0 if α=−2+9β2+4 and det(An)=0 when n≥3.
Thus given (a2,d2)T, we can obtain (a1,d1)T uniquely from the second equality of (7.11),
and then obtain (an,dn)T for n≥3 by the last equality of (7.11).
By the non-triviality of z=z(t), both (7.11) and (7.12) have solutions
{(an,dn)}n=1∞ and {(bn,cn)}n=1∞ respectively.
We assume (7.11) admits a nontrivial solutions.
Then ∑n≥1ancosnt and ∑n≥1dnsinnt are convergent.
Thus, ∑n≥1ansinnt and −∑n≥1dncosnt are convergent too.
Moreover, by the similar structure between equations (7.11) and (7.12),
we can construct a new solution of (7.12) given below if α+1−3β=0,
[TABLE]
Therefore we can build two independent solutions of A(β,e)w=0 as
[TABLE]
If α=−2+9β2+4, then B1 is degenerate.
Note that β=0.
Then the {an,dn} satisfies (7.11), we must have that a2+d2=0.
When a2+d2=0, the (a1,d1) is given by (a1,d1)T=(9β2+4+3β−29β2+4−3β−2,1)d1.
Then {(an,dn)} is obtained by (7.11) and {cn,dn} can be given by (7.12).
Therefore, the claim holds and then this theorem holds.
∎
Proposition 7.4**.**
For any (α~,β~,e)∈REH, i1(ξ~α~,β~,e) is an odd number.
Proof.
When e=0, the conclusion of Proposition 7.4 follows from (1.12).
Now we suppose 0<e<1.
For the given (α~∗,β~∗), we can choose the path that first increase α~ from [math] to α~∗ and then increase β~ from [math] to β~∗.
Suppose there are n intersections with the degenerate surfaces which are defined by (α~∗,β~n∗).
Then by (ii) of Proposition 6.2, we have
[TABLE]
By the proof of Theorem 7.3, every ν1(ξ~α∗,βn∗,e) is even for 1≤k≤n.
Thus by i1(ξ~α∗,β∗,e) is odd by (7.18).
∎
Note that ν1(A~(α~,β~,e))=0 when (α~,β~,e)∈RNH and for (α~,β~,e)∈REH the intersection of 1-degenerates surface and the −1-degenerate surfaces satisfy following theorem.
Proposition 7.5**.**
If (α~,β~,e)∈REH, any 1-degenerate surface and any −1-degenerate surface cannot intersect each other.
That is, for any 0≤e<1, for any n1 and n2∈N,
Πn1(1,e)∩Πn2(−1,e)=∅.
Proof.
If not, suppose 0≤e∗<1 and (α~∗,β~∗) is an
intersection point of some 1-degenerate surface Πn1(1,e∗) and a −1-degenerate surface Πn2(−1,e∗).
Then ν1(ξ~α~∗,β~∗,e∗)≥1 and ν−1(ξ~α~∗,β~∗,e∗)≥1,
and hence σ(ξ~α~∗,β~∗,e∗)={1,1,−1,−1}.
Therefore
there exist b1 and b2 such that ξ~α∗,β∗,e∗(2π)∈Sp(4) satisfies:
[TABLE]
Moreover, by Theorem 7.3, the integer
ν1(ξ~α∗,β∗,e∗)≥1 is even. Together with the fact
ν1(N1(1,b1))=1 when b1=0, we must have b1=0.
There exist two paths ξ~i∈P2π(2) such that we have
ξ~1(2π)=I2, ξ~2(2π)=N1(−1,b2), ξ~α∗,β∗,e∗∼1ξ~1⋄ξ~2, and
i1(ξ~α∗,β∗,e∗)=i1(ξ~1)+i1(ξ~2).
By 1∘ and 2∘ of Lemma 5.6 in Appendix of [38],
both i1(ξ~1) and i1(ξ~2) are odd numbers. Therefore
i1(ξ~α~∗,β~∗,e∗) must be even. But Proposition 7.4 yields
i1(ξ~α∗,β∗,e∗) is an odd number. It is a contradiction. Then this theorem holds.
∎
By 4∘ of Lemma 5.6 in Appendix of [38], i1(R(θ)) is also odd number for θ∈(0,π)∪(π,2π). Then we obtain Theorem 7.6 and omit the proof.
Theorem 7.6**.**
For ω=±1, any ω-degenerate curve and any −1-degenerate
curve cannot intersect each other in REH. That is, for any 0≤e<1, and for any n1 and n2∈N such that Πn1(ω,e)∩Πn2(−1,e)=∅.
Remark 7.7**.**
Note that when α~=0, i.e., α=3β−1, we have the intersection of the 1-degenerate surface and the −1-degenerate.
By Proposition 7.5, the −1- and 1-degenerate surfaces in REH cannot intersect with each other. Therefore, we can order the −1 and 1-degenerate surface, i.e., Σn± and Γn respectively, in the region REH of (α~,β~,e) from left to right as
[TABLE]
where T−1Γn∣e=0=R3,n∗ and T−1Σn−∣e=0=T−1Σn+∣e=0=R3,n+21∗ for n∈N0.
Note that β~=0 is equivalent to Γ0={(α~,β~,e)∣α~>0,β~=0,e∈[0,1)}. According to Proposition 6.2 and (6.26), the 1- and −1-degenerate do intersect. Then we have that Γ0, Σ1− and Σ1+ intersect.
For the given e∈[0,1) and α~∈(0,∞), we have the 1-degenerate points satisfy β~2n(α~,1,e)=β~2n+1(α~,1,e) by Theorem 7.3 and β~2n(α~,−1,e) are the −1-degenerate points. In REH,
[TABLE]
Remark 7.8**.**
If there are some points (α~0,β~0,e0) such that ν1(ξ~α0,β0,e0)≥4.
Then there must exist two different 1-degenerate curves which intersect at (α0,β0,e0).
This contradicts Proposition 7.5.
Thus every 1-degenerate curve has exact geometric multiplicity 2.
Therefore, it is impossible that ξ~α~,β~,e(2π)≈N2(ω,b).
By the list of splitting number in Section 2, we must have that
ξ~α~,β~,e(2π)≈M1⋄M2 where M1 and M2 are two basic normal forms in Sp(2).
By Lemma 3.2 of [38] there exist two paths ξ~1 and
ξ~2 in P2π(2) such that ξ~1(2π)=M1, ξ~2(2π)=M2, ξ~α~,β~,e∼1ξ~1⋄ξ~2,
and i1(ξ~α~,β~,e)=i1(ξ~1)+i1(ξ~2) hold.
Notice that ν1(ξ~α~,β~,e)=0, then ν1(ξ~2)=0 and hence 1∈σ(M2).
Therefore we must have σ(M2)∩U=∅ and α(M2)=0.
Thus, M2=D(2).
Similarly, we have ±1∈σ(M1).
Then by Lemma 5.6 in Appendix 5.2 of [38], we have M1=D(−2) or M1=R(θ) for some θ∈(0,π)∪(π,2π).
If M1=D(−2), by the properties of splitting numbers in Chapter 9 of [20], specially (9.3.3) on p.204,
we obtain i−1(ξ~α~,β~,e)=i1(ξ~α~,β~,e), which contradicts (7.23) and (7.25).
Therefore, we must have M1=R(θ).
If θ∈(0,π), we have
i−1(ξ~α~,β~,e)=i1(ξ~α~,β~,e)−SR(θ)−(e−1θ)+SR(θ)+(e−1θ)=2n.
When θ∈(π,2π), we obtain
i−1(ξ~α~,β~,e)=i1(ξ~α~,β~,e)−SR(θ)−(e−1(2π−θ))+SR(θ)+(e−1(2π−θ))=2n+1 contradicting (7.23).
Therefore, we have θ∈(0,π),
and then ξ~α~,β~,e(2π)≈R(θ)⋄D(2). Thus (i) is proved.
For items (ii)-(iii) and (v)-(vii), we first prove that ξ~α~,β~,e(2π)≈N2(ω,b) is impossible by a method similar to that in
the proof of Theorem 1.5 (ii) or (v). By Lemma 5.3, ξ~α~,β~,e(2π)≈M1⋄M2 must hold.
Then we use the information of ±1-indices, null ±1-indices, Lemma 5.6 and (2.7)
to determine the basic normal forms of M1 and M2. Here the details are omitted.
For (iv), if β~2n+1(α~,−1,e0)=β~2n+2(α~,−1,e0) and β~2n+1(α~,−1,e0)<β~<β~2n+2(α~,−1,e0), by the definition of the degenerate curves, the index and nullity
[TABLE]
Therefore, by (2.7) and the list of splitting number in Section 2, we have that
ξ~α~0,β~0,e0(2π)≈N2(ω,b) for some ω=e−1θ with θ∈(0,π)∪(π,2π) or ξ~α~0,β~0,e0(2π)≈D(λ)⋄D(λ) with λ1, λ2∈R∖{±1}.
If ξ~α~0,β~0,e0(2π)≈N2(ω,b), then we must have that νω(ξ~α~0,β~0,e0(2π))=0.
Then we can find one path γ(t)=(α~,β~(t),te0) for t∈[0,1] linking γ(1)=(α~0,β~(0),e0) with γ(0)=(α~0,β~(1),0) such that νω(ξ~α~0,β~(t),e0(2π))=0 by the continuity of γ~(t).
By Theorem 7.6, we have β~2n+1(α~,−1,te)<β~(t)<β~2n+2(α~,−1,te0).
However, we have that β~2n+1(α~,−1,0)=β~2n+2(α~,−1,0).
Then there must exits a t0 such that β~2n+1(α~,−1,t0e0)=β~(t) or β~(t)=β~2n+2(α~,−1,t0e0).
Then this contradicts with Theorem 7.6.
This yields that ξ~α~0,β~0,e0(2π)≈D(λ1)⋄D(λ2) with λ1, λ2∈R∖{±1}.
Following a similar argument, we have that ξ~α~0,β~0,e0(2π)≈D(2)⋄D(−2).
∎
(i) When m1=m2, by Proposition 6.2 of [15],
the relative equilibria in I1′⊂ΠN are spectrally unstable.
On the other hand, by (2.2) of [7],
R:=I2n−4+D can be considered as
the regularized Hessian of the central configurations.
In fact, for a0∈E which is a central configurations,
then I(a0)=21. With respect to the mass matrix M inner product,
the Hessian of the restriction of the potential to the inertia ellipsoid,
is given by
[TABLE]
and thus
[TABLE]
with n=4.
By (2.85),
(2.89) and β12,0=0, we have
σ(R)={23+9−β,23+9−β,λ3,λ4}.
Thus the eigenvalues of the Hessian at the central configuration
[TABLE]
where μ0>0 is given by (2.75).
Since λ3 is always positive, we must have λ4=−β~<0
when m4 locate on I1′.
By Proposition 4.2 of [15],
all central configurations for m4 in ΠN are non-degenerate.
Thus λ4 does not change its signature
when m4 change its position on ΠN,
and hence λ4=−β~<0 there.
Then we have (α~0,β~0)∈REH.
By Theorem 1.8,
when m4 locates in ΠN,
the ERE is always linearly unstable.
(ii) When m1=m2=m4=0 and m3=1, the central configuration is given by qi are given by q1=0, q2=1, q3=21+−1(23+1)∈∂ΠN.
In this case, we have that α=β=21, i.e., α~=β~=0.
By (i) of Theorem 6.10, for all e∈[0,1), ξ(2π)=ξ~(2π)≈I2⋄N1(1,1) and it is spectrally stable but linearly unstable.
∎
7.3 The ω=±1 degenerate surfaces
In this section, we will discuss that the bifurcation of degenerate curves at e=0.
Therefore, we will use the notation α and β instead of the α~ and β~ and suppose that α≥β>0.
Recall when α>0, A(α,0,e) is positive definite on D(1,2π).
Now we set
[TABLE]
Because A(α,0,e) and 2(1+ecost)3S(t) are self-adjoint, B(β,e) is also self-adjoint.
Also, A(α,0,e)−21 is a compact operator
and 2(1+ecost)3S(t) is a bounded operator,
hence one can apply Theorem 4.8 in p.158 of [13] and conclude that B(α,ω,e) is a compact operator.
Then we have
Lemma 7.9**.**
For 0≤e<1, A(α,β,e) is ω-degenerate if and only if −β1 is an eigenvalue of B(α,ω,e).
Proof.
Suppose A(α,β,e)x=0 holds for some x∈D(1,2π).
Let y=A(α,0,e)21x. Then by (7.32) we obtain
[TABLE]
Conversely, if (β1+B(α,ω,e))y=0,
then x=A(α,0,e)−21y is an eigenfunction of A(α,β,e) belonging to the eigenvalue [math]
by our computations (7.33).
∎
Although e<0 does not have physical meaning, we can extend the fundamental solution to the case e∈(−1,1)
mathematically and all the above results which hold for e>0 and also hold for e<0. By (7.2), the degenerate surface in (α,β,e) can be given by (α,βn(α,1,e))T=T−1(α~,β~n(α,1,e)).
Then we have
Theorem 7.10**.**
For ω∈U, n≥0 and e∈(−1,1), there exist two analytic ω-degenerate surfaces (α,hi(α,ω,e),e) in with i=1,2 such that (α,hi(α,ω,e),e) is between T−1Π2n(1,e) and T−1Π2n+1(1,e). Specially, each hi(α,ω,e) is a really analytic function in e∈(−1,1) and β2n(α,1,e)≤hi(α,ω,e)≤β2n+1(α,1,e) for given α and e. Moreover, ξα,hi(α,ω,e),e(2π) is ω-degenerate for i=1,2.
Therefore, by Lemma 4.3, it shows that, for fixed e∈(−1,1),
exactly two values β=h1(α,ω,e) and h2(α,ω,e) are in the interval [β2n(α,1,e),β2n+1(α,1,e)]
at which (7.33) is satisfied. Then A(α,β,e) at these two values is ω-degenerate.
Note that these two β values are possibly equal to each other at some α and e.
Moreover, (7.35) implies that hi(α,ω,e)=β2n(α,1,e) or β2n+1(α,1,e) for i=1,2.
By (i) of Lemma 4.3, −hi(α,ω,e)1 is an eigenvalue of B(α,e,ω).
Note that B(α,e,ω) is a compact operator and self-adjoint when e is real.
Moreover, it depends analytically on α and e. By Theorem 3.9 of [13],
−hi(α,ω,e)1 is analytic in e for each i∈N. This implies that
both h1(α,ω,e) and h2(α,ω,e) are real analytic functions in α and e.
∎
Theorem 7.11**.**
For ω∈U, every ω-degenerate curve (α,βn(α,ω,e),e) in e∈(−1,1) is a piecewise analytic function.
The set of e∈(−1,1) such that β2n+1(α,ω,e)=β2n+2(α,ω,e) is discrete or equal to the whole interval
(−1,1). In the first case, the functions (α,e)↦βi(α,ω,e) with i=2n+1 and 2n+2 are analytic
for those e when β2n+1(α,ω,e)<β2n+2(α,ω,e). In the second case,
(α,e)↦β2n+1(α,ω,e)=β2n+2(α,ω,e) are analytic everywhere.
By the definition (2.90) of A(α,β,e), we have following results.
[TABLE]
where R(t) is given in (2.90). If e=0, we further have that
[TABLE]
Theorem 7.13**.**
(i)
For n≥0, every 1-degenerate surface starts from the curve R3,n∗ and satisfies
[TABLE]
where p∈R3,n∗ and ∂α∂β(α,−1,0)∣(α,β)∈R3,n∗=9(α+n2+1)2−1α+n2+1.
2. (ii)
If n=0, the two degenerated surfaces Σ1 and Σ2 bifurcate from the curve R3,21∗, with two different tangent spaces satisfy
[TABLE]
where p∈R3,21∗ and ∂α∂β1(α,−1,0)∣e=0=9(α+5/4)2−1α+5/4.
3. (iii)
if n≥1, the two degenerated surfaces Σn+ and Σn− start from R3,n+21∗ and have the same degenerated tangent space
[TABLE]
where p∈Rn+21∗ and ∂α∂βn(α,−1,0)∣e=0=9(α+(n+1/2)2+1)2−4(n+1/2)2α+(n+1/2)2+1.
Proof.
(i) As (7.1), we have that the degenerate surfaces are given by (α,βn(α,1,e),e) and especially when e=0, (α,βn) satisfies α=−(n2+1)+9βn2+4n and α>β.
Let (α,βn(α,1,e),e) be the surface
which intersect with the plane (α,β,0) with the line α=−(n2+1)+9β2+4n. Let
e∈(−ϵ,ϵ) for some small ϵ>0 and xe∈D(1,2π) be the corresponding
eigenvector, that is,
[TABLE]
Recalling (3.37) and (3.38), in the plane e=0, A(α,β,0)
is degenerate when for α=−(n2+1)+9β2+4n and
[TABLE]
with an∈R.
By (3.38), the equation system A(α,β,0)R(t)(ansinnt,cosnt)T=0 reads
[TABLE]
Then by direct computations, an=2nn2+1+α−3β and α=−(n2+1)+9β2+4n.
Therefore by (7.51) and (7.55)-(7.59),
together with (7.55), we have that
[TABLE]
Then we have that for any αn=−(n2+1)+9β2+4n,
[TABLE]
Then we have (i) of this theorem holds.
(ii) As the discussion in (7.1), we have that the degenerate surface is given by (α,β,e)=T−1(α~,β~n(α~,−1,e),e) and especially when e=0, (α,β)∈Rn+21∗.
Similar as the (i) of this proof, let
e∈(−ϵ,ϵ) for some small ϵ>0 and xe∈D(−1,2π) be the corresponding
eigenvector, that is,
[TABLE]
Recalling (3.37) and (3.38), in the plane e=0, A(α,β,0) when (α,β)∈Rn+21∗
is degenerate and the kernel is given by
[TABLE]
with a~n∈R.
By (3.38), the equation system A(α,β,0)R(t)(ansin(n+21)t,cos(n+21)t)T=0 reads
[TABLE]
Then by direct computations, a~n=2(n+21)(n+21)2+1+α−3β and
β=9(α+(n+1/2)2+1)2−4(n+1/2)2.
Therefore, (7.48) and (7.49) hold.
Differentiating both side of (7.49) with respect to e yields (7.50) and (7.51) hold.
Similiar with the calculation (7.52 - 7.54), we have
[TABLE]
and hence
[TABLE]
When n=0, similarly (7.56- 7.58), by direct computations, we have
[TABLE]
where a~0=45+α−3β and β=9(α+5/4)2−1.
Therefore, we have that for n=0, we have that
[TABLE]
By (7.51), for any λ1 and λ2 satisfying λ12+λ22=0,
[TABLE]
This yields that
[TABLE]
where for β>0, a~02(1+α+3β)−(1+α−3β)=23β(9β2+1−3β)=0.
Therefore, we have ∂e∂β1 and ∂e∂β2 satisfy that
[TABLE]
When n=0, the −1-degenerate curve bifurcates at the line R3,21∗ when e=0.
By direct computations, when α≥21, we have that a~02−1=0. Therefore, we have that
[TABLE]
Similarly, for n≥1, by direct computations, we have for i,j∈{1,2}
[TABLE]
Therefore, we have that
[TABLE]
By (7.51) and (7.74),
together with (7.64), we have that for n≥1,
[TABLE]
This yields that
[TABLE]
Then we have (ii) and (iii) of this theorem.
∎
8 The Special Cases with Two Equal Masses
In this section, we apply the discussion in Section 1-7 on the
linear stability of restricted 4-body elliptic solutions.
When m1=m2=m and m3=1−2m. By the symmetry of the central configuration, we can assume that q4,0=21+−1y and y satisfies following central configuration equation.
[TABLE]
where y∈Y1∪Y2∪Y3 with Y1≡(−23,23−1), Y2≡(0,23) and Y3≡(23,23+1) by [15].
By m1=m2=m and m3=1−2m, we have that
[TABLE]
By the definition of α and β by (1.10), we have that in this case α and β are given by
[TABLE]
Plugging (8.2) into (8.3), we have that α(m.y) and β(m,y) can by given by α=α(y) and β=β(y) with y∈Y1∪Y2∪Y3. When y∈Y1, q4,0∈ΠC; when y∈Y2, q4,0∈ΠI; when y∈Y3, q4,0∈ΠN.
Note that when y∈Y3 has been discussed in Theorem 1.3. Then by the assistance of
numerical computations, we have following stability when y∈Y1∪Y2∪Y3.
Theorem 8.1**.**
(i) If y∈Y1, α>3β−1.
There exist y1,1≈−0.6724 and y1,2≈−0.1590 such that when y∈[y1,1,y1,2] and e∈[0,1),
the essential part of the system possesses two pairs of hyperbolic eigenvalues.
When y∈Y1∖[y1,1,y1,2],
(α,β,e)∈RNH.
Furthermore, when e=0, if y∈[y0,23−1) where y0≈−0.1355,
i.e. 0<m≤m0≈0.00270963, the essential part possesses two elliptic eigenvalues and y∈(−23,y0),
we have that (α,β)∈R1 the essential part possesses two hyperbolic eigenvalues.
Then there exists an e∗∈(0,1) such that for e∈[0,e∗), y∈Y1∖(−23,y2,2),
the essential part of the system possesses two pairs of hyperbolic eigenvalues.
(ii) If y∈Y2, we have y2,1≈0.1403, y2,2≈0.1796, y2,3≈0.4224 and y2,4≈0.4937.
When y∈(0,y2,1)∪(y2,4,23), (α,β,e)∈REH and the essential part possesses one pair of hyperbolic eigenvalues and one pair of elliptic eigenvalues.
When y∈(y2,1,y2,2)∪(y2,3,y2,4), (α,β,e)∈RNH.
When y∈(y2,2,y2,3), we have α−3β>0, and the essential part possesses two pairs of hyperbolic eigenvalues.
Especially, when e=0, we have that yˉ2,1≈0.1548 and yˉ2,2≈0.4679.
When y∈(0,y2,1)∪(0,y2,4), (α,β,0)∈R3 and the essential part possesses one pair of hyperbolic eigenvalues one pair of elliptic eigenvalues.
When y∈(y2,1,yˉ2,1)∪(yˉ2,2,y2,4), (α,β,0)∈R4 and the essential part possesses two pairs of hyperbolic eigenvalues.
When y∈(yˉ2,1,yˉ2,2), (α,β,0)∈R1 and the essential part possesses two pairs of hyperbolic eigenvalues.
(iii) If y∈Y3 and e∈[0,1), the essential part possesses one pair of elliptic eigenvalues and one pair of hyperbolic eigenvalues.
Note that the case of (iii) of Theorem 8.1 holds by Theorem 1.3. Then we only prove (i) and (ii) by the assistant of numerical computations
Proof.
(i)
If y∈Y1, the numerical computations show that α>3β−1.
Also α≥3β when y∈[y1,1,y1,2].
By (iii) of Theorem 1.4 , for e∈[0,1), the essential part possesses two pairs of hyperbolic eigenvalues when y∈[y1,1,y1,2].
When y∈Y1∖[y1,1,y1,2], we have (α,β,e)∈RNH.
For α−3β+1=0, there exist two roots which are y1,1≈−0.6724 and y1,2≈−0.1590 such that when y∈[y1,1,y1,2], α≥3β then for e∈[0,1),
the essential part of the system possesses two pairs of hyperbolic eigenvalues. When y∈Y1∖[y1,1,y1,2],
When e=0, the numerical computations show that when y∈(−23,y0) where y0≈−0.1355, α>49β2.
This yields that (α,β,0)∈R1 when y∈(−23,y0).
When y∈[y0,23−1), α≤49β2 and α>3β−1, this yields that (α,β,0)∈R2.
Especially, when y=y0, α<1.
By the continuous of the degenerate region, we have that there exists an e∗∈(0,1) such that when y∈(−23,y2,2),
the two pairs of the eigenvalues are always hyperbolic when e∈[0,e∗).
(ii)
If y∈Y2, there exist y2,1≈0.1403, y2,2≈0.1796, y2,3≈0.4224 and y2,4≈0.4937 such that
when y∈(0,y2,1)∪(y2,4,23), α−3β+1<0. Then (α,β,e)∈REH and the essential part possesses one pair of hyperbolic eigenvalues and one pair of elliptic eigenvalues.
When y∈(y2,1,y2,2)∪(y2,3,y2,4), α−3β+1>0 and α−3β<0.
Then (α,β,e)∈RNH. When y∈(y2,2,y2,3), α−3β>0.
The essential part possesses two pairs of hyperbolic eigenvalues.
Especially, when e=0, we have that yˉ2,1≈0.1548 and yˉ2,2≈0.4679.
When y∈(0,y2,1)∪(0,y2,4),
α−3β+1<0 and α−49β2<0,
this yields that (α,β,0)∈R3 and the essential part possesses one pair of hyperbolic eigenvalues one pair of elliptic eigenvalues.
When y∈(y2,1,yˉ2,1)∪(yˉ2,2,y2,4), α>1, α−3β+1>0 and α−49β2<0,
this yields that (α,β,0)∈R4 and the essential part possesses two pairs of hyperbolic eigenvalues.
This yields that (α,β,0)∈R1 and the essential part possesses two pairs of hyperbolic eigenvalues.
∎
Acknowledgements.
Part of this work was done while B. Liu was visiting the Nankai University and Shandong University; he
sincerely thanks Professor Yiming Long and Professor Xijun Hu for their invitations and inspiring discussion.
The second author thank sincerely Professor Yiming Long for his precious help and valuable comments.
Bibliography41
The reference list from the paper itself. Each links out to its DOI / PubMed record.
1[1] J. Danby, The stability of the triangular Lagrangian point in the general problem of three bodies. Astron. J. 69. (1964) 294-296.
2[2] L. Euler, De motu restilineo trium corporum se mutus attrahentium. Novi Comm. Acad. Sci. Imp. Petrop. 11. (1767) 144-151.
3[3] M. Gascheau, Examen d’une classe d’équations différentielles et application à un cas particulier du problème des trois corps. Comptes Rend. Acad. Sciences. 16. (1843) 393-394.
4[4] W. B. Gordon, A minimizing property of Kepler orbits, American J. of Math. Vol.99, no.5(1977)961-971.
5[5] X. Hu, Y. Long, Y. Ou, Linear stability of the elliptic relative equilibrium with ( 1 + n ) 1 𝑛 (1+n) -gon central configurations in planar n-body problem. ar Xiv:1903.10270[math.DS]
6[6] X. Hu, Y. Long, S. Sun, Linear stability of elliptic Lagrangian solutions of the planar three-body problem via Index Theory. Arch. Ration. Mech. Anal. 213. (2014) 993-1045.
7[7] X. Hu, Y. Ou, An estimate for the hyperbolic region of elliptic Lagrangian solutions in the planar three-body problem. Regul. Chaotic. Dyn. 18(6). (2013) 732-741.
8[8] X.Hu, Y.Ou, Collision index and stability of elliptic relative equilibria in planar n 𝑛 n -body problem. Commum. Math. Phys. 348. (2016) 803-845.