Long-term orbit computations with KS uniformly regular canonical elements with oblateness

Statistics – Computation

Scientific paper

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Canonical Forms, Orbit Calculation, Orbit Perturbation, Runge-Kutta Method, Zonal Harmonics, Artificial Satellites, Circular Orbits, Satellite Tracking

Scientific paper

Uniformly regular canonical Kustaanheimo-Stiefel (1965) elements with earth's oblateness are considered, and computations have been performed to investigate the effects of earth's zonal harmonics and integration step-size variation. The use of recursion formulas for Legendre polynomials allows any number of earth's zonal harmonics to be treated. Numerical integration of the canonical equations is performed via a fixed step-size fourth-order Runge-Kutta-Gill method. The present technique is used to examine the behavior of a 900-km-height near-circular sun-synchronous satellite orbit over a duration of greater than 220 days, along with the effect of higher zonal harmonics on three 990-km-height near-circular orbits with inclinations of 60, 63.2, and 65 degrees.

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