The rectilinear three-body problem as a basis for studying highly eccentric systems

The rectilinear elliptic restricted three-body problem (TBP) is the limiting case of the elliptic restricted TBP when the motion of the primaries is described by a Keplerian ellipse with eccentricity e ′ = 1 , but the collision of the primaries is assumed to be a non-singular point. The rectilinear...

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Veröffentlicht in:	Celestial mechanics and dynamical astronomy 2018, Vol.130 (1), p.1-18, Article 3
Hauptverfasser:	Voyatzis, G., Tsiganis, K., Gaitanas, M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace Technology and Astronautics Astrophysics and Astroparticles Binary stars Classical Mechanics Close Approaches and Collisions in Planetary Systems Collision dynamics Dynamic stability Dynamical Systems and Ergodic Theory Eccentric orbits Geophysics/Geodesy Orbital resonances (celestial mechanics) Orbital stability Orbits Original Article Physics Physics and Astronomy Planetary systems Three body problem
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