Abstract
The path of a point satellite in the field of a point master is called a Kepler orbit. The point master is located in one focus, called the occupied focus (or prime focus) F0 of a Kepler orbit The second focus is unoccupied and is referred to as the vacant focus Fv (Figure 2.1). Kepler orbits are conic sections, whose equation in polar coordinates with origin at the occupied focus is
with p as semi-parameter (or semi-latus rectum), and 6 as (numerical) eccentricity.
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Suggested Reading
Bate, R.R.; D.D. Mueller; J.C. White. Fundamentals of Astrodynamics, Dover, 1971, 455 pp.
Magnus, K. “Kreisel als vielseitige Mittel in Luft- und Raumfahrt”, Zeitschrift für Flugwissenschaften und Weltraumforschung, 2, 4, 1978, pp. 271–227.
Misra, A.K.; V.J. Modi. “Dynamics and Control of Tether-Connected Two-Body Systems — A Brief Review”, Space 2000 (Editor: L. Napolitano), AIAA, New York, 1983, pp. 473–514.
Schiehlen, W.; O. Kolbe. “A Generalization of Kepler Orbits for Large Satellites”, Applied Mechanics (Editors: M. Hetényi; W.G. Vincenti), Springer-Verlag, 1969, pp. 364–381.
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© 1989 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig
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Rimrott, F.P.J. (1989). Kepler Orbits. In: Introductory Orbit Dynamics. Fundamentals and Advances in the Engineering Sciences / Grundlagen und Fortschritte der Ingenieurwissenschaften. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-90338-9_2
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DOI: https://doi.org/10.1007/978-3-322-90338-9_2
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