Analytical model for lunar orbiter

  1. San-Juan, J.F. 1
  2. Abad, A. 2
  3. Elipe, A. 2
  4. Tresaco, E. 2
  1. 1 Universidad de La Rioja
    info

    Universidad de La Rioja

    Logroño, España

    ROR https://ror.org/0553yr311

  2. 2 Universidad de Zaragoza
    info

    Universidad de Zaragoza

    Zaragoza, España

    ROR https://ror.org/012a91z28

Libro:
Advances in the Astronautical Sciences

ISBN: 978-087703544-2

Año de publicación: 2008

Volumen: 130 PART 2

Número: 2

Páginas: 1281-1299

Tipo: Capítulo de Libro

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SCOPUS: 2-s2.0-60349103892 WoS: WOS:000258397800079 GOOGLE SCHOLAR

Resumen

Analytical theories based on Lie-Deprit transforms are used to obtain families of periodic orbits for the problem of an orbiter around the Moon. Low and high orbit models are analyzed. Equilibria of the normalized equations of motion provides the representation of a global portrait of families of frozen orbits depending on values of the inclination, eccentricity and semimajor axis. By means of the inverse transformation it is possible to refine the initial conditions for frozen orbits of a simplified model; these initial conditions may be used as starter of numerical continuation methods when more complex models are considered.

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Información de financiación

Supported by the Spanish Ministry of Science and Technology (Projects # ESP2005- 07107 and # MTM2006-06961).

Financiadores

  • Spanish Ministry of Science and Technology
    • ESP2005-07107
    • MTM2006-06961