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Titlebook: Geostationary Satellites Collocation; Hengnian Li Book 2014 National Defense Industry Press, Beijing and Springer-Verlag Berlin Heidelberg

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樓主
發(fā)表于 2025-3-21 18:18:42 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
書(shū)目名稱(chēng)Geostationary Satellites Collocation
編輯Hengnian Li
視頻videohttp://file.papertrans.cn/385/384089/384089.mp4
概述Focuses on the orbital perturbation analysis for the geostationary orbit.Explains mathematical and physical principle of orbital maneuver and collocation strategies.Presents applications using the alg
圖書(shū)封面Titlebook: Geostationary Satellites Collocation;  Hengnian Li Book 2014 National Defense Industry Press, Beijing and Springer-Verlag Berlin Heidelberg
描述.Geostationary Satellites Collocation. aims to find solutions for deploying a safe and reliable collocation control. Focusing on the orbital perturbation analysis, the mathematical foundations for orbit and control of the geostationary satellite. The mathematical and physical principle of orbital maneuver and collocation strategies for multi geostationary satellites sharing with the same dead band is also stressed. Moreover, the book presents some applications using the above algorithms and mathematical models to help readers master the corrective method for planning station keeping maneuvers. Engineers and scientists in the fields of aerospace technology and space science can benefit from this book..Hengnian Li. is the Deputy Director of State Key Laboratory of Astronautic Dynamics, China..
出版日期Book 2014
關(guān)鍵詞Geostationary Satellite; Orbital Maneuver; Orbital Perturbation; Satellite Collocation; Station Keeping
版次1
doihttps://doi.org/10.1007/978-3-642-40799-4
isbn_softcover978-3-662-51316-3
isbn_ebook978-3-642-40799-4
copyrightNational Defense Industry Press, Beijing and Springer-Verlag Berlin Heidelberg 2014
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沙發(fā)
發(fā)表于 2025-3-21 23:03:50 | 只看該作者
978-3-662-51316-3National Defense Industry Press, Beijing and Springer-Verlag Berlin Heidelberg 2014
板凳
發(fā)表于 2025-3-22 02:20:01 | 只看該作者
Ford: Literature Meets History,The inherent characteristics of the geostationary orbit are introduced in the context of a very simple dynamic problem, and the current status of geostationary satellites is presented simply to arouse two topics, on which this book will focus.
地板
發(fā)表于 2025-3-22 08:34:52 | 只看該作者
Adventure and love: romances in rhyme,There is no absolute stationary orbit for the geostationary satellite to reside in. Special attention we pay in this chapter to the geostationary satellite’s relative motion to the Earth’s rotation motion. We will illustrate the orbit motion of real geostationary satellite with the rotational Earth in inertial space.
5#
發(fā)表于 2025-3-22 09:22:22 | 只看該作者
English Interlanguage MorphologyThe characteristics of the perturbation period of geostationary satellite are analyzed. The spectral decomposing algorithm is established to identify periodical motions from high-precise oscillation ephemeris, and an identification algorithm of periodical motions based on singular value decomposition is presented.
6#
發(fā)表于 2025-3-22 15:30:13 | 只看該作者
https://doi.org/10.1007/978-981-287-071-1The relation between the relative motion of geostationary orbit and the station keeping elements is proposed; the orbit correction equations for the radial, tangential, and normal impulse thrust as well as the continuous thrust are reviewed; and the common properties of in-plane orbit correction and out-plane orbit correction are analyzed.
7#
發(fā)表于 2025-3-22 18:43:58 | 只看該作者
8#
發(fā)表于 2025-3-22 22:24:31 | 只看該作者
The Motion of Geostationary Satellite,There is no absolute stationary orbit for the geostationary satellite to reside in. Special attention we pay in this chapter to the geostationary satellite’s relative motion to the Earth’s rotation motion. We will illustrate the orbit motion of real geostationary satellite with the rotational Earth in inertial space.
9#
發(fā)表于 2025-3-23 02:22:22 | 只看該作者
10#
發(fā)表于 2025-3-23 09:30:55 | 只看該作者
Correction Geostationary Orbit,The relation between the relative motion of geostationary orbit and the station keeping elements is proposed; the orbit correction equations for the radial, tangential, and normal impulse thrust as well as the continuous thrust are reviewed; and the common properties of in-plane orbit correction and out-plane orbit correction are analyzed.
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