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Relativistic effects in the critical inclination problem in artificial satellite theory

✍ Scribed by A. H. Jupp; V. A. Brumberg


Publisher
Springer Netherlands
Year
1991
Tongue
English
Weight
470 KB
Volume
52
Category
Article
ISSN
1572-9478

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✦ Synopsis


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 (i/v/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.


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