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Showing 1 to 2 of 2 (0.073 seconds)Spelling suggestions: "subject:"invariant torus"" "subject:"envariant torus""
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Existência e destruição de toros invariantes, para uma certa família de sistemas Hamiltonianos no R4 / Existence and destruction of invariant torus, for a certain family of Hamiltonian systems in R4Andrade, Julio Cezar de Oliveira 07 June 2019 (has links)
Estudaremos uma fam lia de sistemas hamiltonianos no R 4 , H : R 4 R, satisfazendo certas condi c oes, dependendo de um parametro . Iremos ca- racterizar algumas condi c oes sobre n veis de energia desse sistema, que nos permitem concluir existencia e destrui c ao de toros invariantes, em tais n veis de energia. Al em disso, podemos concluir que o fluxo hamiltoniano, restrito a esses n veis de energia, possui entropia topol ogica positiva. / We will study a family of Hamiltonian Systems in R 4 , satisfying certain conditions, H : R 4 R, depending of a parameter . We will characterize some conditions about the energy levels of this system, which allow us to conclude existence and destruction of invariant torus, at such energy levels. Moreover, we can conclude that the hamiltonian flow, restricted to these energy level, has positive topological entropy.
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Characterization of Quasi-Periodic Orbits for Applications in the Sun-Earth and Earth-Moon SystemsBrian P. McCarthy (5930747) 17 January 2019 (has links)
<div>As destinations of missions in both human and robotic spaceflight become more exotic, a foundational understanding the dynamical structures in the gravitational environments enable more informed mission trajectory designs. One particular type of structure, quasi-periodic orbits, are examined in this investigation. Specifically, efficient computation of quasi-periodic orbits and leveraging quasi-periodic orbits as trajectory design alternatives in the Earth-Moon and Sun-Earth systems. First, periodic orbits and their associated center manifold are discussed to provide the background for the existence of quasi-periodic motion on n-dimensional invariant tori, where n corresponds to the number of fundamental frequencies that define the motion. Single and multiple shooting differential corrections strategies are summarized to compute families 2-dimensional tori in the Circular Restricted Three-Body Problem (CR3BP) using a stroboscopic mapping technique, originally developed by Howell and Olikara. Three types of quasi-periodic orbit families are presented: constant energy, constant frequency ratio, and constant mapping time families. Stability of quasi-periodic orbits is summarized and characterized with a single stability index quantity. For unstable quasi-periodic orbits, hyperbolic manifolds are computed from the differential of a discretized invariant curve. The use of quasi-periodic orbits is also demonstrated for destination orbits and transfer trajectories. Quasi-DROs are examined in the CR3BP and the Sun-Earth-Moon ephemeris model to achieve constant line of sight with Earth and avoid lunar eclipsing by exploiting orbital resonance. Arcs from quasi-periodic orbits are leveraged to provide an initial guess for transfer trajectory design between a planar Lyapunov orbit and an unstable halo orbit in the Earth-Moon system. Additionally, quasi-periodic trajectory arcs are exploited for transfer trajectory initial guesses between nearly stable periodic orbits in the Earth-Moon system. Lastly, stable hyperbolic manifolds from a Sun-Earth L<sub>1</sub> quasi-vertical orbit are employed to design maneuver-free transfer from the LEO vicinity to a quasi-vertical orbit.</div>
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