New periodic orbits in the solar sail three-body problem

J.D. Biggs, T. Waters, C.R. McInnes

Research output: Chapter in Book/Report/Conference proceedingChapter

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Abstract

We identify displaced periodic orbits in the circular restricted three-body problem, wher the third (small) body is a solar sail. In particular, we consider solar sail orbits in the earth-sun system which are high above the exliptic plane. It is shown that periodic orbits about surfaces of artificial equilibria are naturally present at linear order. Using the method of Lindstedt-Poincare, we construct nth order approximations to periodic solutions of the nonlinear equations of motion. In the second part of the paper we generalize to the solar sail elliptical restricted three-body problem. A numerical continuation, with the eccentricity, e, as the varying parameter, is used to find periodic orbits above the ecliptic, starting from a known orbit at e=0 and continuing to the requied eccentricity of e=0.0167. The stability of these periodic orbits is investigated.
Original languageEnglish
Title of host publicationNonlinear Science and Complexity
EditorsJ.A.T. Machado, A.C.J. Luo, R.S. Barbosa, M.F. Silva, L.B. Figueiredo
PublisherSpringer
Pages131-138
Number of pages8
Edition1st
ISBN (Print)9789048198832
Publication statusPublished - Jan 2011
Event2nd Conference on Nonlinear Science and Complexity - Porto, Portugal
Duration: 28 Jul 200831 Jul 2008

Conference

Conference2nd Conference on Nonlinear Science and Complexity
CityPorto, Portugal
Period28/07/0831/07/08

Keywords

  • displaced periodic orbits
  • solar sail
  • restricted three body problem

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