January 26, 2024, Friday, 03:00PM (GMT+03.00, Moscow)
Abstract:
The presentation is dedicated to the methods for constructing quasiperiodic and periodic orbits around the Lagrange points in the circular restricted
three-body problem. Numerical for the calculation and analisys of such orbits, including with the use of artificial intelligence models, are presented.
An analysis of their application domain is performed. Using the developed methods, various families of periodic and quasiperiodic orbits around the Lagrange points,
as well as their stability and bifurcations, are systematically investigated. An example of the use of the developed methods in designing a low-energy transfer
to a polar lunar orbit is presented.