Impulsive transfers between lissajous libration point orbits
A complete methodology for the transfer between two Lissajous orbits around the same collinear equilibrium point is developed making use of the geometry of the phase space around these points. The result of the study gives both strategies to change the amplitudes of the Lissajous orbit and simple pr...
| Autores: | , , |
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| Tipo de recurso: | artículo |
| Fecha de publicación: | 2003 |
| 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:2117/886 |
| Acceso en línea: | https://hdl.handle.net/2117/886 |
| Access Level: | acceso abierto |
| Palabra clave: | Orbital mechanics Dynamics Restricted three body problem Lissajous orbits invariant manifolds transfer orbits exclusion zone Òrbites Mecànica celest Partícules (Física nuclear) Classificació AMS::70 Mechanics of particles and systems::70M20 Orbital mechanics Classificació AMS::70 Mechanics of particles and systems::70F Dynamics of a system of particles, including celestial mechanics |
| Sumario: | A complete methodology for the transfer between two Lissajous orbits around the same collinear equilibrium point is developed making use of the geometry of the phase space around these points. The result of the study gives both strategies to change the amplitudes of the Lissajous orbit and simple procedures to avoid the exclusion zone in an optimal way. The presentation is centered on the linear problem which provides good initial guesses for orbits of small amplitude, likethe requirements for the mission FIRST/Planck of the European Space Agency (ESA), where part of the results of this paper were used for the mission design. |
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