2012/10/01 by S. P. Sosnitskii, Stepan Sosnitskii, Sosnitskii, Stepan
Engineering · Physics and Astronomy · #70F15 #Astro and Planetary Science #Earth and Planetary Astrophysics (astro-ph.EP) #FOS: Physical sciences #Space Satellite Systems and Control #Spacecraft Dynamics and Control #astro-ph.EP #msc:70F15
paper · pdf · doi:10.48550/arxiv.1210.0321
19 pages
arxiv created 2012/10/01 · openalex publication_date 2012/10/01 · arxiv updated 2012/10/02 · openalex created_date 2025/10/24 · openalex updated_date 2026/07/28
For the three-body problem, we consider the Lagrange stability. To analyze the stability, along with integrals of energy and angular momentum, we use relations by the author from Sosnitskii (2005), which band together separately squared mutual distances between bodies (mass points) and squared mutual distances from bodies to the barycenter of the system. In this case, we prove the Lagrange stability theorem, which allows us to define more exactly the character of hyperbolic-elliptic and parabolic-elliptic final evolutions