Dynamics and mission design near libration points, advanced methods for triangular points
The final objective of this work is to understand, analyze and compute the kinds of motion that appear on a vicinity (may be a large vicinity) of the geometrically defined equilateral points of the Earth-Moon system, as a source of possible nominal orbits for future space missions.
| Autores: | , , , |
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| Tipo de recurso: | artículo |
| Fecha de publicación: | 2000 |
| País: | España |
| Institución: | Universitat Politècnica de Catalunya (UPC) |
| Repositorio: | UPCommons. Portal del coneixement obert de la UPC |
| Idioma: | inglés |
| OAI Identifier: | oai:upcommons.upc.edu:2117/1214 |
| Acceso en línea: | https://hdl.handle.net/2117/1214 |
| Access Level: | acceso abierto |
| Palabra clave: | Differentiable dynamical systems Dynamics Orbital mechanics equilateral points Earth-Moon system Sistemes dinàmics diferenciables Teoria ergòdica Partícules (Física nuclear) Òrbites Mecànica celest Classificació AMS::37 Dynamical systems and ergodic theory::37N Applications Classificació AMS::70 Mechanics of particles and systems::70F Dynamics of a system of particles, including celestial mechanics Classificació AMS::70 Mechanics of particles and systems::70M20 Orbital mechanics |
| Sumario: | The final objective of this work is to understand, analyze and compute the kinds of motion that appear on a vicinity (may be a large vicinity) of the geometrically defined equilateral points of the Earth-Moon system, as a source of possible nominal orbits for future space missions. |
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