The use of intermediate orbits for determining minor-body motion

Details The use of intermediate orbits for determining minor-body motion The use of intermediate orbits for determining minor-body motion

Aug 1990

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1990kfnt....6...23m&link_type=abstract

Kinematika i Fizika Nebesnykh Tel (ISSN 0233-7665), vol. 6, July-Aug. 1990, p. 23-28. In Russian.

Statistics

Computation

1

Encke Method, Orbital Mechanics, Perturbation Theory, Three Dimensional Motion, Asteroids, Computerized Simulation, Encke Comet, Planetary Orbits

Scientific paper

The paper presents a method for constructing and using one-parameter intermediate orbits for computing the perturbed motion of a minor body via the Encke technique. The method can also be used to calculate the perturbed differential coefficients in the conditional equations. This method reduces the computation time while retaining the accuracy of the results.

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