Evolution of the satellite's orbit in the Hill's problem taking into account the planet oblateness

Details Evolution of the satellite's orbit in the Hill's problem taking into account the planet oblateness Evolution of the satellite's orbit in the Hill's problem taking into account the planet oblateness

Sep 1974

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1974amst.iafcr....l&link_type=abstract

International Astronautical Federation, International Astronautical Congress, 25th, Amsterdam, Netherlands, Sept. 30-Oct. 5, 197

Computer Science

Numerical Analysis

Elliptical Orbits, Hill Method, Motion Stability, Orbit Perturbation, Satellite Orbits, Equations Of Motion, Numerical Analysis, Numerical Integration, Oblate Spheroids, Orbit Calculation, Orbital Mechanics, Planetary Structure, Runge-Kutta Method

Scientific paper

The evolution of the satellite's orbit under the influence of simultaneous perturbations due to a third body which travels in an elliptical orbit is considered, taking into account effects which occur because of deviations of the planetary field from the properties of a central field. Questions of circular orbit stability are also investigated, giving attention to the transformation of the evolutionary equations and a numerical investigation of stability characteristics.

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