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Titlebook: Dynamics of Natural and Artificial Celestial Bodies; Proceedings of the U Halina Pretka-Ziomek,Edwin Wnuk,David L. Richardso Conference pro

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書目名稱Dynamics of Natural and Artificial Celestial Bodies
副標題Proceedings of the U
編輯Halina Pretka-Ziomek,Edwin Wnuk,David L. Richardso
視頻videohttp://file.papertrans.cn/285/284138/284138.mp4
圖書封面Titlebook: Dynamics of Natural and Artificial Celestial Bodies; Proceedings of the U Halina Pretka-Ziomek,Edwin Wnuk,David L. Richardso Conference pro
描述This volume contains papers presented at the US/European Celestial Mecha- nics Workshop organized by the Astronomical Observatory of Adam Mickiewicz University in Poznan, Poland and held in Poznan, from 3 to 7 July 2000. The purpose of the workshop was to identify future research in celestial mech- anics and encourage collaboration among scientists from eastem and westem coun- tries. There was a full program of invited and contributed presentations on selected subjects and each day ended with a discussion period on a general subject in celestial mechanics. The discussion topics and the leaders were: Resonances and Chaos-A. Morbidelli; Artificial Satellite Orbits-K. T. Alfriend; Near Earth Ob- jects - K. Muinonen; Small Solar System Bodies - I. Williams; and Summary - P. K. Seidelmann. The goal of the discussions was to identify what we did not know and how we might further our knowledge. The size of the meeting and the language differences somewhat limited the real discussion, but, due to the excellence of the different discussion leaders, each of these sessions was very interesting and productive. Celestial Mechanics and Astrometry are both small fields within the general subject
出版日期Conference proceedings 2001
關鍵詞Astrometry; Celestial mechanics; Orbit; Planet; Rigid body; Solar System; artificial satellite; celestial b
版次1
doihttps://doi.org/10.1007/978-94-017-1327-6
isbn_softcover978-90-481-5865-2
isbn_ebook978-94-017-1327-6
copyrightSpringer Science+Business Media Dordrecht 2001
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Changes in Rotational Angular Momentum Due to Gravitational Interactions Between Two Finite Bodies of the change in rotational angular momentum of the non-spherical body are derived over one interaction (i.e. periapsis passage) between the bodies. The estimated changes are expressed in terms of trigonometric functions and generalized Hansen coefficients.
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Formation Flying Satellites: Control by an Astrodynamicistng Hill’s (or Clohessy Wiltshire) equations. Unfortunately the gravitational perturbations destroy the periodicity of the orbits and control will be required to maintain the desired orbits. Since fuel will be one of the major factors limiting the system lifetime it is imperative that fuel consumptio
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Low Energy Transfer to the Moonnsfer. In this paper, we apply the dynamical systems techniques developed in our earlier work to reproduce systematically a Hiten-like mission. We approximate the Sun—Earth—Moon-spacecraft 4-body system as two 3-body systems. Using the invariant manifold structures of the Lagrange points of the 3-bo
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Dissipative Forces and External Resonancesase of external mean motion resonances. The numerical simulations presented are computed by using the 3-dimensional extended Schubart averaging (ESA) integrator developed by Moons (1994) for all mean motion resonances. We complete it by adding the contributions of the dissipative forces. To follow t
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