静止衛星軌道の半径に現れる摂動について [in Japanese] Perturbed Radius of Geosynchronous-Satellite Orbit [in Japanese]
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We analyze theoretically how the radius of geosynchronous orbits would vary owing to the perturbations due to the sun/moon gravity, solar radiation pressure, and the oblate earth. The analysis is simple, as it uses a diagrammatic method to solve near-circular orbital motions. Results are obtained in seven terms of corrections to the radius of non-perturbed ideal orbits. Each correction term is derived, with clear physical meaning, from each component of the perturbing forces.
- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 56(650), 143-148, 2008-03-05
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES