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.
The Three-Body Problem
Modeling,Simulation in Science(Birkhäuser)
2007-01-01
20 pages
Article/Chapter (Book)
Electronic Resource
English
Equilibrium Point , Lagrangian Point , Halo Orbit , Scalar Constant , Advance Composition Explorer Engineering , Automotive Engineering , Mathematical Modeling and Industrial Mathematics , Computational Intelligence , Mathematical and Computational Engineering , Applications of Mathematics , Systems Theory, Control
Wiley | 2024
|Wiley | 2021
|TIBKAT | 1964
|AIAA | 2003
|The Restricted Three-Body Problem
AIAA | 1998
|