The critical inclination problem with small eccentricity View Full Text


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Article Info

DATE

1983-07

AUTHORS

Alan H. Jupp, Ali Y. Abdulla

ABSTRACT

The general theory described in an earlier paper is used to investigate the long-term behavior of the eccentricity and argument of the perigee for Earth satellites which have nearly circular orbits and orbital inclinations in the neighbourhood of the critical value 63°.4. Taking into account the effect of all the zonal harmonics, it is shown that there are just twoTypes of behaviour possible, compared with the six described in the earlier general theory and the four found by Aoki (1963). More... »

PAGES

297-308

References to SciGraph publications

  • 1981-11. The ‘critical inclination’: Another look in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1980-05. The critical inclination problem with small eccentricity in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • 1981-10. Orbits near critical inclination, including lunisolar perturbations in CELESTIAL MECHANICS AND DYNAMICAL ASTRONOMY
  • Identifiers

    URI

    http://scigraph.springernature.com/pub.10.1007/bf01232195

    DOI

    http://dx.doi.org/10.1007/bf01232195

    DIMENSIONS

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