Abstract:In this work we present a method to bound the di usion near an elliptic equilibrium point of a periodically time-dependent Hamiltonian system. The method is based on the computation of the normal form (up to a certain degree) of that Hamiltonian, in order to obtain an adequate number of (approximate) rst integrals of the motion. Then, bounding the variation of those integrals with respect to time provides estimates of the di usion of the motion.The example used to illustrate the method is the Elliptic Spatial … Show more
“…Finally, you have to modify the input/output routines accordingly. This is what we have done in [28] or [50], for the case of a periodically perturbed Hamiltonian system.…”
Section: Extensionssupporting
confidence: 69%
“…Of course, in order to produce realistic diusion times one needs to have H 1 as small as it can be. Astandard way of producing the splitting (1) is by means of a normal form calculation: H 0 is the normal form and H 1 the corresponding remainder (see [14] and also [43] and [28]).…”
Section: Dynamics Near An Elliptic Equilibrium Pointmentioning
confidence: 99%
“…This will produce a high order approximation to the results wanted that, in many cases, are goodenough for pratical purposes. On the other hand, it is possible to derive rigorous estimates on the size of this remainder so one can obtain bounds on the error of the results obtained with the truncated series (see [43], [28] or [32] for numerical examples of this).…”
This paper deals with the eective computation of normal forms, centre manifolds and rst integrals in Hamiltonian mechanics. These kind of calculations are very useful since they allow, for instance, to give explicit estimates on the diusion time or to compute invariant tori. The approach presented here is based on using algebraic manipulation for the formal series but taking numerical coecients for them. This, jointly with a very ecient implementation of the software, allows big savings in both memory and execution time of the algorithms if we compare with the use of commercial algebraic manipulators. The algorithms are presented jointly with their C/C++ implementations, and they are applied to some concrete examples coming from celestial mechanics.
“…Finally, you have to modify the input/output routines accordingly. This is what we have done in [28] or [50], for the case of a periodically perturbed Hamiltonian system.…”
Section: Extensionssupporting
confidence: 69%
“…Of course, in order to produce realistic diusion times one needs to have H 1 as small as it can be. Astandard way of producing the splitting (1) is by means of a normal form calculation: H 0 is the normal form and H 1 the corresponding remainder (see [14] and also [43] and [28]).…”
Section: Dynamics Near An Elliptic Equilibrium Pointmentioning
confidence: 99%
“…This will produce a high order approximation to the results wanted that, in many cases, are goodenough for pratical purposes. On the other hand, it is possible to derive rigorous estimates on the size of this remainder so one can obtain bounds on the error of the results obtained with the truncated series (see [43], [28] or [32] for numerical examples of this).…”
This paper deals with the eective computation of normal forms, centre manifolds and rst integrals in Hamiltonian mechanics. These kind of calculations are very useful since they allow, for instance, to give explicit estimates on the diusion time or to compute invariant tori. The approach presented here is based on using algebraic manipulation for the formal series but taking numerical coecients for them. This, jointly with a very ecient implementation of the software, allows big savings in both memory and execution time of the algorithms if we compare with the use of commercial algebraic manipulators. The algorithms are presented jointly with their C/C++ implementations, and they are applied to some concrete examples coming from celestial mechanics.
“…The model has applications in space mission design [14,15], explains symbolic dynamics phenomena observed in trajectories of comets [18], and can be used for the study of diffusion estimates [16,17]. All of the above are associated with dynamics along invariant manifolds of the system.…”
We present a computer assisted proof of existence of a family of Lyapunov orbits which stretches from L2 (the collinear libration point between the primaries) up to half the distance to the smaller primary in the Jupiter-Sun planar circular restricted three body problem. We then focus on a small family of Lyapunov orbits with energies close to comet Oterma and show that their associated invariant manifolds intersect transversally. Our computer assisted proof provides explicit bounds on the location and on the angle of intersection.
“…Our approach to averaging differs from the dominant one [AKN97,Nei84,GH,Hale,SVM,JS,L], which following the pioneering work of ( [BM, BZ]) used suitable coordinates changes to control the influence of the rapidly oscillating perturbation.…”
For the Srzednicki-Wójcik equation, the planar nonautonomous ODE parameterized by κ ∈ R,using averaging we show how the region of hyperbolicty grows with |κ|.Based on this we give bounds on the sizes of bounded orbits.
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