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Periodic orbits for space-based reflectors in the circular restricted three-body problem
(2017-05-01)
The use of space-based orbital reflectors to increase the total insolation of the Earth has been considered with potential applications in night-side illumination, electric power generation and climate engineering. Previous ...
Peculiar trajectories around the Lagrangian equilateral points
(Elsevier B.V., 2007-01-01)
In the present work we analyse the behaviour of a particle under the gravitational influence of two massive bodies and a particular dissipative force. The circular restricted three body problem, which describes the motion ...
Peculiar trajectories around the Lagrangian equilateral points
(Elsevier B.V., 2007-01-01)
In the present work we analyse the behaviour of a particle under the gravitational influence of two massive bodies and a particular dissipative force. The circular restricted three body problem, which describes the motion ...
Distribución superficial de impactos en Iapetus originada por el remanente de una colisión
(Asociación Argentina de Astronomía, 2015)
Mediante el Problema Circular de Tres Cuerpos Restricto Saturno–Iapetus se analizan posibles distribuciones de impactos sobre la superficie de Iapetus, originadas a partir de considerar una población de baja energía generada ...
Peculiar trajectories around the Lagrangian equilateral points
(Elsevier B.V., 2014)
Chaotic Dynamics in a Low-Energy Transfer Strategy to the Equilateral Equilibrium Points in the Earth-Moon System
(World Scientific Publ Co Pte Ltd, 2015-05-01)
In the frame of the equilateral equilibrium points exploration, numerous future space missions will require maximization of payload mass, simultaneously achieving reasonable transfer times. To fulfill this request, low-energy ...
Natural formations at the Earth-Moon triangular point in perturbed restricted problems
(Elsevier B.V., 2015-07-01)
Previous studies for small formation flying dynamics about triangular libration points have determined the existence of regions of zero and Minimum Relative Radial Acceleration with respect to the nominal trajectory, that ...
Spacecraft motion around artificial equilibrium points
(2018-02-01)
The main goal of this paper is to describe the motion of a spacecraft around an artificial equilibrium point in the circular restricted three-body problem. The spacecraft is under the gravitational influence of the Sun and ...
A semi-relativistic approach to the circular restricted three-body problem and a numerical experiment around the 3 : 2 resonance
(Iop Publishing LtdBristolInglaterra, 2006)