Relativistic effects in the critical inclination problem in artificial satellite theory View Full Text


Ontology type: schema:ScholarlyArticle     


Article Info

DATE

1991-12

AUTHORS

A. H. Jupp, V. A. Brumberg

ABSTRACT

It is well known that in artifical satellite theory special techniques must be employed to construct a formal solution whenever the orbital inclination is sufficiently close to the critical value cos−1 (1/√5). In this article the authors investigate the consequences of introducing certain relativistic effects into the motion of a satellite about an oblate primary. Particular attention is paid to the critical inclination(s), and for such critical motions an appropriate method of solution is formulated. More... »

PAGES

345-353

References to SciGraph publications

  • 1969-03. Canonical transformations depending on a small parameter in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1986-06. Unsolved problems of celestial mechanics in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1989-06. Relativistic effects in the motion of artificial satellites: The oblateness of the central body II in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1984-09. The ideal resonance problem a comparison of two formal solutions I in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1987-03. Relativistic effects in the motion of artificial satellites: The oblateness of the central body I in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1985-10. The ideal resonance problem, a comparison of two formal solutions, II in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1987-06. The ideal resonance problem a comparison of two formal solutions III in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1987-03. The critical inclination problem — 30 years of progress in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • Identifiers

    URI

    http://scigraph.springernature.com/pub.10.1007/bf00048450

    DOI

    http://dx.doi.org/10.1007/bf00048450

    DIMENSIONS

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