Three body problem
By Alain Chenciner. Scholarpedia, 2007
556 citations recorded by the source corpus.
An isolated system consisting of two point masses exerting forces on one another — which is usually referred to as a two-body problem — can always be converted into an equivalent one-body problem. In particular, we can exactly solve a dynamical system containing two gravitationally interacting point masses. What about a system containing three gravitationally interacting point masses? Despite hundreds of years of research, no exact solution of this famous problem — which is generally known as the three-body problem — has ever been found. It is, however, possible to make some progress by restricting the problem’s scope.
Subfields: Aerospace Engineering, Astronomy and Astrophysics
View Paper: https://www.semanticscholar.org/paper/372650bb915cd7d0ccdb2ae9bfc27140cf6a1b94
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In Aerospace Engineering
In Astronomy and Astrophysics
Citations in the corpus
- Eccentric Black Hole Mergers Forming in Globular Clusters (2017, unknown): “Its value can be analytically estimated by using that the normalized orbital energy distribution of binaries assembled in three-body interactions approximately follows [45, 57],”
- Post-oligarchic Evolution of Protoplanetary Embryos and the Stability of Planetary Systems (2007, background): “Based on the results from qualitative studies of the general three-body problem (e.g., Marchal 1990), Gladman (1993) investigated the stability of the two planet systems both analytically and numerically.”
- The Eccentric Kozai-Lidov Effect and Its Applications (2016, background): “…phenomena, it was limited to a narrow parts of the parameter space (favoring close to perpendicular initial orientation between the two orbits, e.g., Marchal 1990; Morbidelli 2002; Valtonen and Karttunen 2006; Fabrycky and Tremaine 2007) and produced only moderate eccentricity excitations.”
- Suppression of extreme orbital evolution in triple systems with short-range forces (2014, methodology): “Harrington (1968); Marchal et al. (1990); Krymolowski & Mazeh (1999); Ford et al. (2000b); Blaes et al. (2002) have derived the orbit-averaged Hamiltonian to octupole order and used the resulting equation of motion to explore some aspects of the evolution of triples.”
- Earthformer: Exploring Space-Time Transformers for Earth System Forecasting (2022, methodology): “We choose N 3 in the experiments so that the digits will follow the chaotic 3 -body motion [25].”
- ECCENTRICITY GROWTH AND ORBIT FLIP IN NEAR-COPLANAR HIERARCHICAL THREE-BODY SYSTEMS (2013, methodology): “2 degree due to the “Kozai resonance” (Thomas & Morbidelli 1996). Recently, Naoz et al. (2011, 2012) showed that relaxing either one of these assumptions, (i.e., an eccentric outer orbit, or non-negligible mass binary members) leads to qualitatively different behavior. In this case the z-component o”
- THE ECCENTRIC KOZAI MECHANISM FOR A TEST PARTICLE (2011, methodology): “To do so, we use the secular octupole Hamiltonian of Ford et al. (2000), which was apparently first derived by Harrington (1968) (as cited by Harrington 1969; see also Marchal 1990 and Krymolowski & Mazeh 1999 for derivations).”