Effective Stability of the equilateral Lagrangepoints
Effective Stability of the equilateral Lagrangepoints
Disciplines
Mathematics (50%); Physics, Astronomy (50%)
Keywords
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Nekhoroshev Theory,
Exponential Stability,
Sympletic Mappings,
Birkhoff Normal Forms,
Trojan-type Motion,
Elliptic Three Body Problen
Contrary to the KAM theorem (Kolmogorov 1954, Arnold 1963, Moser 1962), which asserts stability for all times of those orbits of a nonlinear dynamical system, with initial conditions belonging to a Cantor set of tori of non-zero measure, exponential stability is of much greater interest from the physical point of view, because it can be applied to all orbits in open domains of the phase space, whether they lie on an invariant torus or not. The corresponding theorem proven by Nekhoroshev (1977) defines stability regions for a finite time T in both, regular and chaotic domains of the phase space. If the life-time of the physical system is shorter than the stability time derived from the Nekhoroshev estimates of the region, one can definitely say that orbits belonging to this region are stable from the practical point of view. An already known example of the Lagrangian equilateral configuration in our solar system, where Nekhoroshev estimates are applicable, is the population of Trojan asteroids around the equilibrium points L4 and L5 of the Sun-Jupiter system. The Trojans are in the 1:1 mean motion resonance with Jupiter and their motions and semimajor axes oscillate around those of Jupiter as mean values. While moving around the Sun, the Trojans perform librating motions around Jupiter`s L4 or L5 point, located at 60 before and after Jupiter on Jupiter`s orbit. All investigations of the Nekhoroshev stability of the Trojan type motion up to now were based on the circular restricted three body problem. This circular model is a great simplification of the real physical system that neglects all phenomena due to the ellipticity of the orbit of Jupiter and its secular changes due to the presence of the other planets. Therefore it is a mathematical challenge and represents a physically very interesting problem to generalize the Nekhoroshev estimates of the size of the stable region. Based on the method of Hadjimetriou we will develop a set of corresponding 4 dimensional mappings of the Trojan-type motion for different eccentricities of the perturbing body to make our results applicable also to Trojan planets in exosolar systems. Using the theory of Birkhoff normal forms, we will find an explicit form of the remainder of the mappings, which will directly lead us to suitable Nekhoroshev estimates of the Trojan-type motion. Thus our work is a logical next step on getting closer to more realistic applications of Nekhoroshev theory in celestial mechanics.
Contrary to the KAM theorem (Kolmogorov 1954, Arnold 1963, Moser 1962), which asserts stability for all times of those orbits of a nonlinear dynamical system, with initial conditions belonging to a Cantor set of tori of non-zero measure, exponential stability is of much greater interest from the physical point of view, because it can be applied to all orbits in open domains of the phase space, whether they lie on an invariant torus or not. The corresponding theorem proven by Nekhoroshev (1977) defines stability regions for a finite time T in both, regular and chaotic domains of the phase space. If the life-time of the physical system is shorter than the stability time derived from the Nekhoroshev estimates of the region, one can definitely say that orbits belonging to this region are stable from the practical point of view. An already known example of the Lagrangian equilateral configuration in our solar system, where Nekhoroshev estimates are applicable, is the population of Trojan asteroids around the equilibrium points L4 and L5 of the Sun-Jupiter system. The Trojans are in the 1:1 mean motion resonance with Jupiter and their motions and semimajor axes oscillate around those of Jupiter as mean values. While moving around the Sun, the Trojans perform librating motions around Jupiter`s L4 or L5 point, located at 60 before and after Jupiter on Jupiter`s orbit. All investigations of the Nekhoroshev stability of the Trojan type motion up to now were based on the circular restricted three body problem. This circular model is a great simplification of the real physical system that neglects all phenomena due to the ellipticity of the orbit of Jupiter and its secular changes due to the presence of the other planets. Therefore it is a mathematical challenge and represents a physically very interesting problem to generalize the Nekhoroshev estimates of the size of the stable region. Based on the method of Hadjimetriou we will develop a set of corresponding 4 dimensional mappings of the Trojan-type motion for different eccentricities of the perturbing body to make our results applicable also to Trojan planets in exosolar systems. Using the theory of Birkhoff normal forms, we will find an explicit form of the remainder of the mappings, which will directly lead us to suitable Nekhoroshev estimates of the Trojan-type motion. Thus our work is a logical next step on getting closer to more realistic applications of Nekhoroshev theory in celestial mechanics.
- Universität Wien - 100%
Research Output
- 253 Citations
- 6 Publications
-
2011
Title Prospects of the detection of circumbinary planets with Kepler and CoRoT using the variations of eclipse timing DOI 10.1111/j.1365-2966.2011.18594.x Type Journal Article Author Schwarz R Journal Monthly Notices of the Royal Astronomical Society Pages 2763-2770 Link Publication -
2009
Title Dynamics of possible Trojan planets in binary systems DOI 10.1111/j.1365-2966.2009.15248.x Type Journal Article Author Schwarz R Journal Monthly Notices of the Royal Astronomical Society Pages 2085-2090 Link Publication -
2009
Title The dynamics of Neptune Trojan – I. The inclined orbits DOI 10.1111/j.1365-2966.2009.15203.x Type Journal Article Author Zhou L Journal Monthly Notices of the Royal Astronomical Society Pages 1217-1227 Link Publication -
2009
Title An Introduction to Common Numerical Integration Codes Used in Dynamical Astronomy DOI 10.1007/978-3-642-04458-8_9 Type Book Chapter Author Eggl S Publisher Springer Nature Pages 431-480 -
2010
Title The dynamics of Neptune Trojans – II. Eccentric orbits and observed objects? DOI 10.1111/j.1365-2966.2010.17566.x Type Journal Article Author Zhou L Journal Monthly Notices of the Royal Astronomical Society Pages 1849-1860 Link Publication -
2008
Title Nekhoroshev stability at L4 or L5 in the elliptic-restricted three-body problem – application to Trojan asteroids DOI 10.1111/j.1365-2966.2007.12794.x Type Journal Article Author Lhotka C Journal Monthly Notices of the Royal Astronomical Society Pages 1165-1177 Link Publication