Wednesday, June 22 |
07:30 - 09:00 |
Breakfast (Restaurant Hotel Hacienda Los Laureles) |
09:00 - 09:40 |
Alberto Boscaggin: Periodic solutions to relativistic Kepler problems. ↓ By using both geometrical and variational methods, we investigate existence, multiplicity and variational characterization of periodic solutions of (forced) relativistic Kepler problems in the plane. Joint works with W. Dambrosio (Torino), G. Feltrin and D. Papini (Udine). (Zoom) |
09:40 - 10:20 |
Gian Marco Canneori: Symbolic dynamics for the anisotropic N-centre problem. ↓ We consider the planar N-centre problem of Celestial Mechanics in which we associate to every centre a homogeneous anisotropic potential. As a peculiar difference with classical Newtonian potentials, the attraction field generated by every centre is no longer radial and the rotational symmetry is lost. As a consequence, the integrability of the system is completely lost and regularization methods such as the Levi-Civita transform no longer succeed in this contest. The total energy is still a first integral of the system and our main result is the existence of bounded periodic trajectories in negative energy shells. This is obtained employing both variational and perturbation methods. In particular, we show that over a certain threshold on the homogeneity degree of the potentials all the solution trajectories of this system are collision-less. Consequently, the existence of a symbolic dynamics for the system is deduced, which is enriched by the important role played by the minimal central configurations of the potentials taken into account. This is a joint work with Vivina Barutello and Susanna Terracini. (Conference Room San Felipe) |
10:20 - 11:00 |
Gabriella Pinzari: Recent results on the three—body problem. ↓ The planar Euler problem has a first integral which, in the limit when the mass of one of the attracting centers vanishes, has a pendulum-like dynamics. On the other hand, the three—body problem Hamiltonian differs from the one of the Euler problem for a kinetic
term. Therefore, the natural question arises whether, in the three—body problem there is a memory of the dynamics of the Euler problem. We show that, under suitable assumptions, this is the case. This talk is based on joint works with Qinbo Chen, Jerome Daquin and Sara Di Ruzza. (Zoom) |
11:00 - 11:30 |
Coffee Break (Conference Room San Felipe) |
11:30 - 12:10 |
Ariadna Farres: On the geometry of Station-Keeping around Libration Point Orbits. ↓ Over the years Libration Point orbits have become relevant in space applications, as the regions around the L1 and L2 points in the Circular Restricted Three-Body (CRTBP) are ideal for space weather missions like the Space Weather Follow-On (SWFO) or deep space observations like the Roman Space Telescope (RST) or the James Webb Space Telescope (JWST). It is well known that Libration point orbits are unstable and require routine station-keeping maneuvers to remain in orbit. Over the years different station-keeping strategies have been proposed, each of them with different objective functions.
In this talk, we want to describe the geometry behind some of these strategies making use of the Floquet mode reference frame to compare them. We focus on two different strategies, the widely used by NASA approach, x-axis velocity constraint at the plain crossing, and the Floquet mode approach. The first approach looks for the delta-v required to ensure that at the 4th plane crossing Vx = 0, ensuring the spacecraft to orbit around the Libration point. On the other hand, the Floquet mode approach looks for the delta-v that cancels the unstable, bringing the trajectory close to the stable manifold or a reference orbit. As we will see, both approaches have some basic geometrical common features, even when they are compared using high-order techniques.
Understanding the geometry of these strategies allows us to study the optimality of the delta-v maneuvers analytically. We will show why the minimum thrust direction is close to the position components of the stable eigenvector. We also describe the dependence of the maneuver size as a function of the thrust direction and provide a tool to describe the impact of mission constraints in the thrust directions. Moreover, the geometric interpretation of station-keeping allows us to envision strategies that can help to mitigate the impact of mission constraints, such as actively biasing the delta-v maneuvers when the spacecraft can only thrust away from the sun.
This is a joint work with Chen Gao, Josep Masdemont, Gerard Gomez, Dave Folta and Cassandra Webster (Geometrical Analysis of Station-Keeping Strategies About Libration Point Orbits, JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS Vol. 45, No. 6, June 2022) (Zoom) |
12:10 - 12:50 |
Jaime Paradela: Arnold Diffusion in the Restricted Planar Three Body Problem. ↓ Consider the RPE3BP with any mass ratio μ ∈ (0, 1/2) and any eccentricity ∈ (0, 1). We build orbits along which the angular momentum of the massless body becomes unbounded as t → ∞. The construction relies on an Arnold diffusion mechanism by designing a transition chain of periodic orbits. For that, we identify an invariant manifold at infinity and prove that its four dimensional stable and unstable manifolds intersect transversally along two different homoclinic manifolds. These homoclinic manifolds define two scattering maps which encode the dynamics along the heteroclinic orbits. We prove that they can be combined to build a sequence of periodic orbits connected by heteroclinics along which the angular momentum grows unboundedly. One of the main diculties is that the splitting angle between the stable and unstable manifolds is exponentially small with respect to the angular momentum and therefore Melnikov theory cannot be applied. This is joint work with Marcel Guardia and Tere Seara. (Conference Room San Felipe) |
12:50 - 13:30 |
Joan Gimeno: Computation of invariant manifolds of high dimensional tori in Celestial Mechanics. ↓ In this talk, we present a procedure to compute reducible tori and their un/stable manifolds. The method is efficient and parallelizable and it scales to multiple shooting approaches. To illustrate the results we are going to focus in a perturbed model of the Earth-Moon system with five natural frequencies leading to high dimensional quasi-periodic solutions of the perturbed R3BP. This was a joint work with A. Jorba, B. Nicolas, and E. Olmedo. (Zoom) |
13:30 - 15:00 |
Lunch (Restaurant Hotel Hacienda Los Laureles) |
19:00 - 21:00 |
Dinner (Restaurant Hotel Hacienda Los Laureles) |