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Zero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon system

Autor
Salazar, F.; Masdemont, J.J.; Gomez Muntané, Gerard; Macau, E.E.N.; Winter, O.
Tipus d'activitat
Article en revista
Revista
Advances in space research
Data de publicació
2014-11-01
Volum
54
Número
9
Pàgina inicial
1838
Pàgina final
1857
DOI
https://doi.org/10.1016/j.asr.2014.07.018 Obrir en finestra nova
Repositori
http://hdl.handle.net/2117/24992 Obrir en finestra nova
URL
http://www.sciencedirect.com/science/article/pii/S0273117714004748# Obrir en finestra nova
Resum
Assume a constellation of satellites is flying near a given nominal trajectory around L-4 or L-5 in the Earth-Moon system in such a way that there is some freedom in the selection of the geometry of the constellation. We are interested in avoiding large variations of the mutual distances between spacecraft. In this case, the existence of regions of zero and minimum relative radial acceleration with respect to the nominal trajectory will prevent from the expansion or contraction of the constellat...
Citació
Salazar, F. [et al.]. Zero, minimum and maximum relative radial acceleration for planar formation flight dynamics near triangular libration points in the Earth-Moon system. "Advances in space research", 01 Novembre 2014, vol. 54, núm. 9, p. 1838-1857.
Paraules clau
Circular Restricted Three Body Problem, ELLIPTIC ORBITS, Earth-Moon system, Formation flight of satellites, MISSION, MOTION, PERIODIC-ORBITS, QUADRATIC DRAG, Residual acceleration, STABILITY, Stable Lagrangian points, Zero Relative Radial Acceleration
Grup de recerca
SD - Sistemes Dinàmics de la UPC

Participants