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Charged three-body system with arbitrary masses near conformal invariance
(Amer Physical Soc, 2009-11-01)
Within an adiabatic approximation to the three-body Coulomb system, we study the strength of the leading-order conformaly invariant attractive dipole interaction produced when a slow charged particle q(3) (with mass m(3)) ...
Charged three-body system with arbitrary masses near conformal invariance
(Amer Physical Soc, 2009-11-01)
Within an adiabatic approximation to the three-body Coulomb system, we study the strength of the leading-order conformaly invariant attractive dipole interaction produced when a slow charged particle q(3) (with mass m(3)) ...
Quantum propagator for some classes of three-dimensional three-body systems
(2006-05-01)
In this work we solve exactly a class of three-body propagators for the most general quadratic interactions in the coordinates, for arbitrary masses and couplings. This is done both for the constant as the time-dependent ...
Quantum propagator for some classes of three-dimensional three-body systems
(2006-05-01)
In this work we solve exactly a class of three-body propagators for the most general quadratic interactions in the coordinates, for arbitrary masses and couplings. This is done both for the constant as the time-dependent ...
Lagrange points
(2016)
Lagrange points
(2011)
Developing the precessing Inclined Bi-Elliptical Four-Body Problem with Radiation Pressure to search for orbits in the triple asteroid 2001SN263
(2016-02-15)
Space missions to visit small bodies of the Solar System are important steps to improve our knowledge of the Solar System. Usually those bodies do not have well known characteristics, as their gravity field, which make the ...
Three-body problem, its Lagrangian points and how to exploit them using an alternative transfer to L4 and L5
(Springer, 2012-10-01)
An alternative transfer strategy to send spacecraft to stable orbits around the Lagrangian equilibrium points L4 and L5 based in trajectories derived from the periodic orbits around L1 is presented in this work. The ...
Three-body problem, its Lagrangian points and how to exploit them using an alternative transfer to L4 and L5
(Springer, 2012-10-01)
An alternative transfer strategy to send spacecraft to stable orbits around the Lagrangian equilibrium points L4 and L5 based in trajectories derived from the periodic orbits around L1 is presented in this work. The ...