Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects

Peláez Álvarez, Jesús and Bombardelli, Claudio and Lara, M. and Lucas, Fernando R. and Sanjurjo Rivo, Manuel and Curreli, D. and Lorenzini, Enrico C. and Scheeres, D. (2011). Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects. In: "22nd International Symposium on Space Flight Dynamics - 22nd ISSFD", 28/02/2011 - 04/03/2011, Säo José dos Campos, Brasil. pp. 73-81.

Description

Title: Dynamic stabilization of L2 periodic orbits using attitude-orbit coupling effects
Author/s:
  • Peláez Álvarez, Jesús
  • Bombardelli, Claudio
  • Lara, M.
  • Lucas, Fernando R.
  • Sanjurjo Rivo, Manuel
  • Curreli, D.
  • Lorenzini, Enrico C.
  • Scheeres, D.
Item Type: Presentation at Congress or Conference (Article)
Event Title: 22nd International Symposium on Space Flight Dynamics - 22nd ISSFD
Event Dates: 28/02/2011 - 04/03/2011
Event Location: Säo José dos Campos, Brasil
Title of Book: 22nd International Symposium on Space Flight Dynamics - 22nd ISSFD
Date: 28 February 2011
Subjects:
Freetext Keywords: roto-orbital dynamics, Hill problem, periodic orbits, stability
Faculty: E.T.S.I. Aeronáuticos (UPM)
Department: Física Aplicada a la Ingeniería Aeronáutica [hasta 2014]
Creative Commons Licenses: Recognition - No derivative works - Non commercial

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Abstract

Numerical explorations show how the known periodic solutions of the Hill problem are modified in the case of the attitude-orbit coupling that may occur for large satellite structures. We focus on the case in which the elongation is the dominant satellite’s characteristic and find that a rotating structure may remain with its largest dimension in a plane parallel to the plane of the primaries. In this case, the effect produced by the non-negligible physical length is dynamically equivalent to the perturbation produced by an oblate central body on a mass-point satellite. Based on this, it is demonstrated that the attitude-orbital coupling of a long enough body may change the dynamical characteristics of a periodic orbit about the collinear Lagrangian points.

More information

Item ID: 21139
DC Identifier: http://oa.upm.es/21139/
OAI Identifier: oai:oa.upm.es:21139
Deposited by: Memoria Investigacion
Deposited on: 28 Mar 2014 19:05
Last Modified: 21 Apr 2016 11:14
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