A database of high precision trivial choreographies for the planar three-body problem I. Hristov1 R. Hristova12 I. Puzynin3

2025-04-28 0 0 7.83MB 10 页 10玖币
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A database of high precision trivial
choreographies for the planar three-body problem
I. Hristov1, R. Hristova1,2, I. Puzynin3,
T. Puzynina3, Z. Sharipov3, and Z. Tukhliev3
1Faculty of Mathematics and Informatics, Sofia University "St. Kliment Ohridski",
Sofia, Bulgaria
ivanh@fmi.uni-sofia.bg
2Institute of Information and Communication Technologies, Bulgarian Academy of
Sciences, Sofia, Bulgaria
3Meshcheryakov Laboratory of Information Technologies, Joint Institute for Nuclear
Research, Dubna, Russia
zarif@jinr.ru
Abstract. Trivial choreographies are special periodic solutions of the
planar three-body problem. In this work we use a modified Newton’s
method based on the continuous analog of Newton’s method and a high
precision arithmetic for a specialized numerical search for new trivial
choreographies. As a result of the search we computed a high precision
database of 462 such orbits, including 397 new ones. The initial condi-
tions and the periods of all found solutions are given with 180 correct
decimal digits. 108 of the choreographies are linearly stable, including 99
new ones. The linear stability is tested by a high precision computing of
the eigenvalues of the monodromy matrices.
Keywords: Three-body problem ·Trivial choreographies ·Modified
Newton’s method, ·High precision arithmetic
1 Introduction
A choreography is a periodic orbit in which the three bodies move along one
and the same trajectory with a time delay of T/3, where Tis the period of
the solution. A choreography is called trivial if it is a satellite (a topological
power) of the famous figure-eight choreography [1,2]. Trivial choreographies are
of special interest because many of them are expected to be stable like the figure-
eight orbit. About 20 new trivial choreographies with zero angular momentum
and bodies with equal masses are found in [3,4,5], including one new linearly
stable choreography, which was the first found linearly stable choreography after
the famous figure-eight orbit. Many three-body choreographies (345) are also
found in [6], but they are with nonzero angular momentum and an undetermined
topological type.
In our recent work [7] we made a purposeful (on a small domain of initial
conditions) numerical search for figure-eight satellites (not necessarily choreogra-
phies). For numerical search we used a modification of Newton’s method with a
arXiv:2210.00594v1 [math.NA] 2 Oct 2022
2 I. Hristov, R. Hristova, I. Puzynin et al.
larger domain of convergence. The three-body problem is well known with the
sensitive dependence on the initial conditions. To overcome the obstacle of deal-
ing with this sensitivity and to follow the trajectories correctly for a long time,
we used as an ODE solver the high order multiple precision Taylor series method
[8,9,10]. As a result we found over 700 new satellites with periods up to 300 time
units, including 45 new choreographies. 7 of the newly found choreographies are
shown to be linearly stable, bringing the number of the known linearly stable
choreographies up to 9.
This work can be regarded as a continuation of our recent work [7]. Now
we make a specialized numerical search for new trivial choreographies by using
the permuted return proximity condition proposed in [4]. We consider the same
searching domain and the same searching grid step as in [7]. Considering pretty
long periods (up to 900 time units), which are much longer than those in the
previous research, allows us to compute a high precision database of 462 trivial
choreographies, including 397 new ones. 99 of the newly found choreographies
are linearly stable, so the number of the known linearly stable choreographies
now rises to 108.
2 Differential equations describing the bodies motion
The bodies are with equal masses and they are treated as point masses. A planar
motion of the three bodies is considered. The normalized differential equations
describing the motion of the bodies are:
¨ri=
3
X
j=1,j6=i
(rjri)
krirjk3, i = 1,2,3.(1)
The vectors ri,˙rihave two components: ri= (xi, yi),˙ri= ( ˙xi,˙yi). The system
(1) can be written as a first order one this way:
˙xi=vxi,˙yi=vyi,˙vxi=
3
X
j=1,j6=i
(xjxi)
krirjk3,˙vyi=
3
X
j=1,j6=i
(yjyi)
krirjk3, i = 1,2,3
(2)
We solve numerically the problem in this first order form. Hence we have a vector
of 12 unknown functions X(t)=(x1, y1, x2, y2, x3, y3, vx1, vy1, vx2, vy2, vx3, vy3)>.
Let us mention that this first order system actually coincides with the Hamilto-
nian formulation of the problem.
We search for periodic planar collisionless orbits as in [3,4]: with zero angular
momentum and symmetric initial configuration with parallel velocities:
(x1(0), y1(0)) = (1,0),(x2(0), y2(0)) = (1,0),(x3(0), y3(0)) = (0,0)
(vx1(0), vy1(0)) = (vx2(0), vy2(0)) = (vx, vy)
(vx3(0), vy3(0)) = 2(vx1(0), vy1(0)) = (2vx,2vy)
(3)
The velocities vx[0,1], vy[0,1] are parameters. We denote the periods of the
orbits with T. So, our goal is to find triplets (vx, vy, T )for which the periodicity
condition X(T) = X(0) is fulfilled.
摘要:

Adatabaseofhighprecisiontrivialchoreographiesfortheplanarthree-bodyproblemI.Hristov1,R.Hristova1;2,I.Puzynin3,T.Puzynina3,Z.Sharipov3,andZ.Tukhliev31FacultyofMathematicsandInformatics,SoaUniversity"St.KlimentOhridski",Soa,Bulgariaivanh@fmi.uni-sofia.bg2InstituteofInformationandCommunicationTechnol...

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分类:图书资源 价格:10玖币 属性:10 页 大小:7.83MB 格式:PDF 时间:2025-04-28

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