ArticlePublisher preview available

The orbital evolution of the Sun–Jupiter–Saturn–Uranus–Neptune system on long time scales

Authors:
To read the full-text of this research, you can request a copy directly from the authors.

Abstract and Figures

The averaged semi-analytical motion theory of the four-planetary problem is constructed up to the third order in planetary masses and the sixth degree in the orbital eccentricities and inclinations. The second system of Poincaré elements and the Jacobi coordinate system are used for the construction of the Hamiltonian expansion. The averaged Hamiltonian is obtained in the third approximation by the Hori–Deprit method. All analytical transformations are performed by using CAS Piranha. The constructed equations of motion in averaged elements are numerically integrated by the different methods for the giant planets of the Solar System over a time interval of up to 10 Gyr. The planetary motion is quasi-periodic, and the short-term perturbations of the orbital elements conserve small values in the modeling process. The comparison of obtained amplitudes and periods of the change of the orbital elements with numerical motion theories shows an excellent agreement with them. The properties of the planetary motion are given. The short-periodic perturbations and the precision of the integration are estimated.
This content is subject to copyright. Terms and conditions apply.
Astrophys Space Sci (2020) 365:144
https://doi.org/10.1007/s10509-020-03855-w
ORIGINAL ARTICLE
The orbital evolution of the Sun–Jupiter–Saturn–Uranus–Neptune
system on long time scales
Alexander Perminov1·Eduard Kuznetsov1
Received: 22 January 2020 / Accepted: 12 August 2020 / Published online: 27 August 2020
© Springer Nature B.V. 2020
Abstract The averaged semi-analytical motion theory of
the four-planetary problem is constructed up to the third or-
der in planetary masses and the sixth degree in the orbital ec-
centricities and inclinations. The second system of Poincaré
elements and the Jacobi coordinate system are used for the
construction of the Hamiltonian expansion. The averaged
Hamiltonian is obtained in the third approximation by the
Hori–Deprit method. All analytical transformations are per-
formed by using CAS Piranha.
The constructed equations of motion in averaged ele-
ments are numerically integrated by the different methods
for the giant planets of the Solar System over a time inter-
val of up to 10 Gyr. The planetary motion is quasi-periodic,
and the short-term perturbations of the orbital elements con-
serve small values in the modeling process. The compari-
son of obtained amplitudes and periods of the change of the
orbital elements with numerical motion theories shows an
excellent agreement with them. The properties of the plane-
tary motion are given. The short-periodic perturbations and
the precision of the integration are estimated.
Keywords Celestial mechanics ·Methods: analytical ·
Methods: numerical ·Planet–star interactions ·Planets and
satellites: dynamical evolution and stability ·Planets and
satellites: individual: Jupiter, Saturn, Uranus, Neptune
BA. Perminov
perminov12@yandex.ru
E. Kuznetsov
eduard.kuznetsov@urfu.ru
1Ural Federal University, 51 Lenin Avenue, 620000 Ekaterinburg,
Russia
1 Introduction
This article is related to the problem of the study of the or-
bital evolution of planetary systems. The averaged equations
of motion are constructed analytically up to the third degree
in the small parameter for the case of the four-planetary sys-
tem. The ratio of the sum of planetary masses to the mass of
the star plays the role of the small parameter in the problem
(from now on denoted μ).
The orbital evolution of the four-planet Sun–Jupiter
Saturn–Uranus–Neptune system is considered in this article.
The mass of the Solar System’s giant planets is smaller than
the mass of the Sun to three orders (the value of the small pa-
rameter). The mass of the terrestrial planets is smaller than
the giant planets’ one by three orders also. Therefore the in-
fluence of the terrestrial planets on the orbital motion of the
giant planets is insignificant. On the contrary, catastrophic
changes in the motion of the giant planets can lead to the de-
struction of the whole Solar System. So, the giant-planetary
approximation of the Solar System is sufficient for the in-
vestigation of the dynamical evolution and stability on long
time scales.
It is convenient to use the equations of motion in aver-
aged orbital elements for the study of dynamical evolution
on long time scales. The use of averaged elements allows
one to sufficiently increase the integration step of the equa-
tions of motion and, consequently, reduce the integration
time. The Solar System’s orbital evolution on cosmogonic
time scales was first studied analytically in the 19th century.
The modern averaging theories are developed based on ideas
of Lagrange, Laplace, and Gauss.
The main point of averaging methods is the elimination
from the equations of motion all short-periodic terms whose
periods are comparable with or less than the circulation pe-
riods of the planets. The fast variables of the problem give
Content courtesy of Springer Nature, terms of use apply. Rights reserved.
... In [7] the authors analyzed dynamical evolution of young pairs of asteroids in close orbits. In work [8] evolution of planetary systems was studied. The averaged equations of motion was derived analytically up to third power of a small parameter for the case of a four planetary system. ...
... Note that λ i is calculated after integrating equations (8). ...
... In equations (8), by reducing the left and right sides of the equation by a common multiplier ω 1 (f m 00 a 1 ) 1/4 = const, we obtain the evolution equations in dimensionless quantities. ...
Article
Full-text available
In celestial mechanics and astrodynamics, the study of the dynamical evolution of exoplanetary systems is the relevant topics. For today more than 3,000 exoplanetary systems are known. In this paper, we study the dynamic evolution of extrasolar systems, when the leading factor of evolution is the variability of the masses of gravitating bodies. The problem of spherically symmetric bodies with variable masses is considered in a relative coordinate system, this bodies inter-gravitating according to Newton's law. The quasi-elliptical motions of planets whose orbits do not intersect during evolution are investigated. It is believed that the mass of bodies under consideration varies isotropically by various known laws with different velocities. The mass of the parent star is considered to be the most massive than its planets and the origin of the relative coordinate system is in the center of the parent star.. Due to the variability of the masses, the differential equations of motion become non-autonomous and the task is difficult. The problem is investigated by methods of perturbation theory. The canonical perturbation theory based on a periodic motion over a quasi-canonical section is used. Canonical equations of motion are obtained in analogues of the second Poincare system, which are effective in the case when the analogues of eccentricities and the analogues of the inclination of the orbital plane of planets are sufficiently small. The secular perturbations of the planets, which determine the behavior of the orbital parameters over long time intervals, are studied. The evolutionary equations of many planetary systems with isotropically varying masses in analogues of the second system of Poincare variables are derived in an analytical form which are obtained using the Wolfram Mathematica computer algebra system. This takes into account the effects of the decreasing mass of the parent star and the growth of the masses of the planets due to the accretion of matter from the remnants of the protoplanetary disk. For the three-planetary problem of four bodies with variable masses, the evolutionary equations in dimensionless variables are obtained explicitly. In the future, these results will be used to study the dynamics of the three-planet system K2-3 in the non-stationary stage of its evolution.
... В настоящее время известно около 5 500 внесолнечных планет в более чем 4 000 планетных системах, причем около 900 из этих систем многопланетные. Авторами в работе [1] построена и апробирована численно-аналитическая теория движения для четырехпланетной задачи, позволяющая исследовать динамическую эволюцию внесолнечных планетных систем (с числом планет до 4) на космогонических интервалах времени. Согласно базе данных exoplanet.eu ...
Conference Paper
Full-text available
The Hamiltonian of the eight-planetary problem is written in the Jacobi coordinates. It is expanded into a Poisson series in the small parameter and orbital elements of the second Poincare system. The Hamiltonian is averaged by the Hori - Deprit method of the second order in a small parameter. The motion equations in the averaged elements and the functions for the change of variables for the transition between osculating and averaged elements are constructed.
... The transformation between osculating and averaged orbital elements is performed by the functions for the change of variables. An application of the constructed four-planetary motion theory to modeling the orbital evolution of the solar system's giant planets is considered by authors in Perminov & Kuznetsov (2018, 2020 for the second and third orders of theory correspondingly. ...
Article
Full-text available
This article is devoted to studying the dynamical evolution and orbital stability of compact extrasolar three-planetary system GJ 3138. In this system, all semimajor axes are less than 0.7 au. The modeling of planetary motion is performed using the averaged semi-analytical motion theory of the second order in planetary masses, which the authors construct. Unknown and known with errors orbital elements vary in allowable limits to obtain a set of initial conditions. Each of these initial conditions is applied for the modeling of planetary motion. The assumption about the stability of observed planetary systems allows to eliminate the initial conditions leading to excessive growth of the orbital eccentricities and inclinations and to identify those under which these orbital elements conserve moderate values over the whole modeling interval. Thus, it becomes possible to limit the range of possible values of unknown orbital elements and determine their most probable values in terms of stability.
Article
В работе исследуется динамическая эволюция компактной трехпланетной системы Kepler-51. Анализируются возможные резонансные состояния системы и проводится поиск потенциальных цепочек резонансов средних движений. С помощью программного комплекса Posidonius исследуется динамическая эволюция системы на интервале времени 100 млн лет с учетом приливного взаимодействия. Также для различных начальных значений эксцентриситетов, наклонов, аргументов перицентров и долгот восходящих узлов орбит проводится моделирование динамической эволюции планетной системы в рамках численно-аналитической теории движения. Показано, что компактная планетная система Kepler-51 не является резонансной. При начальных условиях, соответствующих массам и элементам орбит планет, определенным из наблюдений с учетом их погрешностей, эволюция системы является устойчивой и регулярной на исследуемом интервале 100 млн лет.
Article
Full-text available
We investigate the secular evolution of a four-body planetary system, where two planets mo v e around a binary star configuration on quasi-elliptic orbits. It is assumed that the masses of all bodies can change isotropically at different rates and the bodies attract each other according to Newton's law of universal gravitation. The purpose of this work is to investigate an influence of variability of the masses of the binary stars and their planets on the dynamical evolution of the planetary system. We consider the case of small eccentricities and inclinations of the bodies orbits and assume that their orbits do not intersect during e volution. Dif ferential equations of the perturbed motion in the osculating analogues of canonical Poincar é elements were obtained in a general case of the many-body problem with variable masses in our previous work. Here we solve these equations numerically and investigate the secular evolution of some fictitious circumbinary 2-planet system under assumption that the two stars of the binary system lose their masses independently at different rates. In order to demonstrate the dynamical features of the equations we use the known parameters of the TOI-1338 system. Comparing the results of calculations in the cases of constant and variable masses, we show that the isotropic variability of the masses of bodies can influence substantially the secular perturbation of the orbital elements.
Chapter
Modeling the dynamics of the exoplanetary system TRAPPIST with seven bodies of variable mass moving around a central parent star along quasi-elliptic orbits is discussed. The bodies are assumed to be spherically symmetric and attract each other according to Newton’s law of gravitation. In this case, the leading factor of dynamic evolution of the system is the variability of the masses of all bodies. The problem is analyzed in the framework of Hamiltonian’s formalism and the differential equations of motion of the bodies are derived in terms of the osculating elements of aperiodic motion on quasi-conic sections. These equations can be solved numerically but their right-hand sides contain many oscillating terms and so it is very difficult to obtain their solutions over long time intervals with necessary precision. To simplify calculations and to analyze the behavior of orbital parameters over long time intervals we replace the perturbing functions by their secular parts and obtain a system of the evolutionary equations composed by 28 non-autonomous linear differential equations of the first order. Choosing some realistic laws of mass variations and physics parameters corresponding to the exoplanetary system TRAPPIST, we found numerical solutions of the evolutionary equations. All the relevant symbolic and numeric calculations are performed with the aid of the computer algebra system Wolfram Mathematica.KeywordsNon-stationary many-body problemIsotropic change of massSecular perturbationsEvolution equationsPoincaré variables
Article
Full-text available
This article is related to the problem of the construction of planetary motion theory. We have expanded the Hamiltonian of the four-planetary problem into the Poisson series in osculating elements of the second Poincare system. The series expansion is constructed up to the third degree of the small parameter. The averaging procedure of the Hamiltonian is performed by the Hori–Deprit method. It allows to eliminate short-periodic perturbations and sufficiently increase time step of the integration of the equations of motion. This method is based on Lie transformation theory. The equations of motion in averaged elements are constructed as the Poisson brackets of the averaged Hamiltonian and corresponding orbital element. The transformation between averaged and osculating elements is given by the change-variable functions, which are obtained in the second approximation of the Hori–Deprit method. We used computer algebra system Piranha for the implementation of the Hori–Deprit method. Piranha is an echeloned Poisson series processor authored by F. Biscani. The properties of the obtained series are discussed. The numerical integration of the equations of motion is performed by Everhart method for the Solar system’s giant planets.
Article
Full-text available
We investigate the long-time stability of the Sun-Jupiter-Saturn-Uranus system by considering a planar secular model, that can be regarded as a major refinement of the approach first introduced by Lagrange. Indeed, concerning the planetary orbital revolutions, we improve the classical circular approximation by replacing it with a solution that is invariant up to order two in the masses; therefore, we investigate the stability of the secular system for rather small values of the eccentricities. First, we explicitly construct a Kolmogorov normal form, so as to find an invariant KAM torus which approximates very well the secular orbits. Finally, we adapt the approach that is at basis of the analytic part of the Nekhoroshev's theorem, so as to show that there is a neighborhood of that torus for which the estimated stability time is larger than the lifetime of the Solar System. The size of such a neighborhood, compared with the uncertainties of the astronomical observations, is about ten times smaller.
Article
The averaged semi-analytical motion theory of second order in planetary masses for the four-planet problem has been constructed. The Hamiltonian and equations of motion are given in Jacobi coordinates and written in elements of the second Poincaré system. The eccentric and oblique Poincaré orbital elements are conserved in the equations of motion up to third order. The orbital evolution of the three-planet system HD 39194 and the four-planet systems HD 141399 and HD 160691 (μ Ara) is considered. The numerical integration of the equations of motion was carried out for a set of initial conditions, in which unknown orbital elements and orbital elements that are known from observations with some uncertainty were varied within admissible limits. The ranges of variation of the orbital elements are determined as a function of the initial conditions. The assumption that the observed planetary systems are stable can be used to exclude initial conditions leading to extreme growth in the orbital eccentricities and inclinations. Initial conditions for which the orbital elements remain small over the entire modeling interval are identified. A method that can be used to narrow the range of possible values of the unknown orbital elements and identify most probable values from the point of view of stability is shown.
Article
The four-planet problem is solved by constructing an averaged semi-analytical theory of secondorder motion by planetary masses. A discussion is given of the results obtained by numerical integration of the averaged equations of motion for the Sun–Jupiter–Saturn–Uranus–Neptune system over a time interval of 10 Gyr. The integration is based on high-order Runge–Kutta and Everhart methods. The motion of the planets is almost periodic in nature. The eccentricities and inclinations of the planetary orbits remain small. Short-period perturbations remain small over the entire interval of integration. Conclusions are drawn about the resonant properties of the motion. Estimates are given for the accuracy of the numerical integration.
Conference Paper
In this paper, we consider the using of the computer algebra system Piranha as applied to the study of the planetary problem. Piranha is an echeloned Poisson series processor, which is written in C++ language. It is new, specified, high-efficient program for analytical transformations of polynomials, Fourier and Poisson series. We used Piranha for the expansion of the Hamiltonian of four-planetary problem into the Poisson series and the construction of motion equations by the Hori–Deprit method. Both of these algorithms are briefly presented in this work. Different properties of the series representation of the Hamiltonian and motion equations are discussed.
Article
We consider an algorithm to construct averaged motion equations for four-planetary systems by means of the Hori–Deprit method. We obtain the generating function of the transformation, change-variable functions and right-hand sides of the equations of motion in elements of the second Poincaré system. Analytical computations are implemented by means of the Piranha echeloned Poisson processor. The obtained equations are to be used to investigate the orbital evolution of giant planets of the Solar system and various extrasolar planetary systems.
Article
Finding a common origin for various celestial bodies, especially the relations between meteoroid streams, comets and asteroids (possibly extinct comets), remains one of the important problems in Solar system astronomy. Different criteria, starting with one by Southworth and Hawkins, have been used for this purpose. Ideally, they must represent some kind of metric in a five-dimensional space of orbits. Unfortunately, they are not ideal. The majority of the criteria have been examined by us. It turns out that they all represent pseudometrics for which the triangle axiom is not fulfilled. Besides this, they are inapplicable if at least one of the orbits is circular. We propose metrics free of all the aforementioned drawbacks. In addition, the metric properties of three factor-spaces, where orbits are identified irrespective of the values of node longitudes, pericentre arguments or both, are examined. The results are applied to the problem of searching for minor bodies of the Solar system with a common origin. The relationship between comet 96P/Machholz 1 and asteroid 2003EH1, as well as that between comet 2P/Encke and asteroid 2004TG10, has been proved. Using all criteria considered and the new metrics leads to practically identical results. This is explained by the fact that only close and essentially non-circular orbits were analysed. Besides this, the measure of orbit triples for which the triangle axiom failed is likely small, though this problem has not been examined yet.
Article
Scitation is the online home of leading journals and conference proceedings from AIP Publishing and AIP Member Societies
Article
The Hamiltonian of the N-planetary problem is written in the Jacobi coordinates using the second system of Poincare elements. The Hamiltonian is expanded into the Poisson series for the four-planet system. The computer algebra system Piranha is used for analytical transformations. Obtained expansions provide the Hamiltonian expression accuracy up to the third degree of the small parameter for giant planets of the Solar System and up to the second degree of the small parameter for extrasolar planetary systems. The ratio of sums of masses of the planets to the star mass can be selected as a small parameter.