On the optimal station keeping control of halo orbits

C. Simó; G. Gómez; J. Llibre; R. Martínez; J. Rodríguez

doi:10.1016/0094-5765(87)90175-5

On the optimal station keeping control of halo orbits

C. Simó, G. Gómez, J. Llibre, R. Martínez, J. Rodríguez

Departamento de Matemáticas

Producción científica: Contribución a una revista › Artículo › Investigación › revisión exhaustiva

145 Citas (Scopus)

Resumen

Techniques for computing and controlling a halo orbit are considered in this paper. It presents a semi-analytical theory for the halo orbits in the Restricted Three Bodies Problem (RTBP), that is valid and amenable to computation to any order. Results are presented up to order 11. The Floquet modes of the monodromy matrix are used to define a local optimal control procedure through the concepts of projection and gain functions. © 1987.

Idioma original	Inglés
Páginas (desde-hasta)	391-397
Publicación	Acta Astronautica
Volumen	15
DOI	https://doi.org/10.1016/0094-5765(87)90175-5
Estado	Publicada - 1 ene 1987

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10.1016/0094-5765(87)90175-5

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https://www.scopus.com/pages/publications/0022737897

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title = "On the optimal station keeping control of halo orbits",

abstract = "Techniques for computing and controlling a halo orbit are considered in this paper. It presents a semi-analytical theory for the halo orbits in the Restricted Three Bodies Problem (RTBP), that is valid and amenable to computation to any order. Results are presented up to order 11. The Floquet modes of the monodromy matrix are used to define a local optimal control procedure through the concepts of projection and gain functions. {\textcopyright} 1987.",

author = "C. Sim{\'o} and G. G{\'o}mez and J. Llibre and R. Mart{\'i}nez and J. Rodr{\'i}guez",

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doi = "10.1016/0094-5765(87)90175-5",

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T1 - On the optimal station keeping control of halo orbits

AU - Simó, C.

AU - Gómez, G.

AU - Llibre, J.

AU - Martínez, R.

AU - Rodríguez, J.

PY - 1987/1/1

Y1 - 1987/1/1

N2 - Techniques for computing and controlling a halo orbit are considered in this paper. It presents a semi-analytical theory for the halo orbits in the Restricted Three Bodies Problem (RTBP), that is valid and amenable to computation to any order. Results are presented up to order 11. The Floquet modes of the monodromy matrix are used to define a local optimal control procedure through the concepts of projection and gain functions. © 1987.

AB - Techniques for computing and controlling a halo orbit are considered in this paper. It presents a semi-analytical theory for the halo orbits in the Restricted Three Bodies Problem (RTBP), that is valid and amenable to computation to any order. Results are presented up to order 11. The Floquet modes of the monodromy matrix are used to define a local optimal control procedure through the concepts of projection and gain functions. © 1987.

UR - https://www.scopus.com/pages/publications/0022737897

U2 - 10.1016/0094-5765(87)90175-5

DO - 10.1016/0094-5765(87)90175-5

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VL - 15

SP - 391

EP - 397

JO - Acta Astronautica

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ER -

On the optimal station keeping control of halo orbits

Resumen

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Huella

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