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.
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.
| Original language | English |
|---|---|
| Pages (from-to) | 199-215 |
| Number of pages | 17 |
| Journal | Celestial Mechanics and Dynamical Astronomy |
| Volume | 110 |
| Issue number | 3 |
| DOIs | |
| Publication status | Published - Jul 2011 |
Keywords
- Non-Keplerian orbits
- circular restricted three-body problem
- artificial equilibria
- artificial satellites
- displaced orbits
Fingerprint
Dive into the research topics of 'Displaced non-Keplerian orbits using impulsive thrust'. Together they form a unique fingerprint.Projects
- 1 Finished
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VISIONSPACE - VISIONARY SPACE SYSTEMS: ORBITAL DYNAMICS AT EXTREMES OF SPACECRAFT LENGTH SCALE (ERC ADVANCED GRANT)
McInnes, C. (Principal Investigator)
European Commission - FP7 - European Research Council
1/02/09 → 30/09/14
Project: Research
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