The method of finding periodic three-body orbits

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SUMMARY

This discussion focuses on determining periodic orbits in equal-mass three-body Newtonian gravitational problems. The key method involves confining the three bodies within a zero angular momentum space, where the total angular momentum sums to zero (∑Iw=0). Participants emphasize the importance of calculating initial conditions based on mass, orbital speed, and radius, as well as understanding algebraic symmetries and free group elements to categorize orbit families into distinct classes.

PREREQUISITES
  • Understanding of Newtonian gravitational problems
  • Familiarity with angular momentum concepts
  • Knowledge of gravitational force calculations
  • Basic grasp of algebraic symmetries and group theory
NEXT STEPS
  • Research methods for calculating initial conditions in three-body problems
  • Learn about zero angular momentum space in gravitational systems
  • Explore algebraic symmetries in dynamical systems
  • Study free group elements and their applications in orbit classification
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Astronomers, physicists, and mathematicians interested in celestial mechanics and the dynamics of three-body systems.

Pefgjk
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Hello everyone!

I'm trying to get a deeper understanding on how to determine those periodic orbits in the equal-mass three-body Newtonian gravitational problems. The most general idea I know is to confine the three bodies into a zero angular momentum space, which sounds vague to me. What is the more detailed computational job here, to derive the numerical initial conditions?

Also, what is the general idea of "algebraic symmetries", and "free group elements", that are used to sort the "families" of orbits into distinct "classes".

Thanks in advance!
 
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Zero angular momentum space seems to mean that the sum of the angular momentums ∑Iw=0. That means you have to know/figure out the mass, orbit speed, and radius.

You could also calculate the gravitational force between the bodies knowing their masses and distance between them and set that equal to the centripetal force to find the velocity/orbit.
 

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