Displaced non-Keplerian orbits using impulsive thrust

Colin McInnes

Research output: Contribution to journalArticle

9 Citations (Scopus)

Abstract

This paper investigates new families of displaced, highly non-Keplerian orbits in
the two-body problem and artificial equilibria in the circular restricted three-body problem. The families of orbits presented extend prior work by using periodic impulses to generate displaced orbits rather than continuous thrust. The new displaced orbits comprise a sequence of individual Keplerian arcs whose intersection is continuous in position, with discontinuities in velocity removed using impulses. For frequent impulses the new families of orbits approximate continuous thrust non-Keplerian orbits found in previous studies. To generate approximations to artificial equilibria in the circular restricted three-body problem, periodic impulses are used to generate a sequence of connected three-body arcs which begin and terminate at a fixed position in the rotating frame of reference. Again, these families of orbits reduce to the families of artificial equilibria found using continuous thrust.
LanguageEnglish
Pages199-215
Number of pages17
JournalCelestial Mechanics and Dynamical Astronomy
Volume110
Issue number3
DOIs
Publication statusPublished - Jul 2011

Fingerprint

thrust
Orbits
Orbit
orbits
Impulse
impulses
Restricted Three-body Problem
three body problem
Arc of a curve
arcs
two body problem
discontinuity
Terminate
family
intersections
Discontinuity
Rotating
Intersection
Family
Approximation

Keywords

  • Non-Keplerian orbits
  • circular restricted three-body problem
  • artificial equilibria
  • artificial satellites
  • displaced orbits

Cite this

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Displaced non-Keplerian orbits using impulsive thrust. / McInnes, Colin.

In: Celestial Mechanics and Dynamical Astronomy, Vol. 110, No. 3, 07.2011, p. 199-215.

Research output: Contribution to journalArticle

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