Orbits in a generalized two-body problem

C.R. McInnes

Research output: Contribution to journalArticle

26 Citations (Scopus)

Abstract

The two-body problem is a well-known case of the general central force problem with an attractive, inverse square force. However, there are forms of spacecraft propulsion, such as solar sails and minimagnetospheric plasmapropulsion, which generate a repulsive, inverse square force. Because this force can be modulated, a more general central force problem is then formed. Such a problem is investigated and the families of orbits available using both forward integration and an inverse approach are explored. Both are used to explore various modes of transfer between circular coplanar orbits and to determine strategies for escape.
LanguageEnglish
Pages743-749
Number of pages6
JournalJournal of Guidance, Control and Dynamics
Volume26
Issue number5
Publication statusPublished - 2003

Fingerprint

two body problem
Orbits
spacecraft
Spacecraft propulsion
Solar sails
Orbit
orbits
spacecraft propulsion
solar sails
Coplanar
circular orbits
Spacecraft
escape
family

Keywords

  • guidance systems
  • orbits
  • space travel
  • solar sails

Cite this

McInnes, C.R. / Orbits in a generalized two-body problem. In: Journal of Guidance, Control and Dynamics. 2003 ; Vol. 26, No. 5. pp. 743-749.
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Orbits in a generalized two-body problem. / McInnes, C.R.

In: Journal of Guidance, Control and Dynamics, Vol. 26, No. 5, 2003, p. 743-749.

Research output: Contribution to journalArticle

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