Abstract
To model the problem of three bodies in mutual gravitational attaction and present its general solution by Lagrange.To develop the restricted three-body problem for modeling the flight of a spacecraft under the gravitational influence of two massive bodies.To discuss the solvability, equilibrium points, and numerical solutions of the restricted three-body problem with examples of earth-moon-spacecraft trajectories.
Cite
CITATION STYLE
APA
The three-body problem. (2007). In Modeling and Simulation in Science, Engineering and Technology (Vol. 27, pp. 173–192). Springer Basel. https://doi.org/10.1007/978-0-8176-4438-3_7
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