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Titlebook: Algorithms for Satellite Orbital Dynamics; Lin Liu Textbook 2023 Nanjing University Press 2023 Orbit elements.Orbit determination.Satellit

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樓主
發(fā)表于 2025-3-21 16:30:52 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
期刊全稱Algorithms for Satellite Orbital Dynamics
影響因子2023Lin Liu
視頻videohttp://file.papertrans.cn/154/153235/153235.mp4
發(fā)行地址Presents basic theory, equations, and calculation of satellite orbits, for students.Provides calculations for design, tracking, prediction, and adjustment of satellite orbit or deep spacecrafts.Contai
學(xué)科分類Springer Series in Astrophysics and Cosmology
圖書封面Titlebook: Algorithms for Satellite Orbital Dynamics;  Lin Liu Textbook 2023 Nanjing University Press 2023 Orbit elements.Orbit determination.Satellit
影響因子This book highlights the fundamental physics of orbit theory, dynamical models, methods of orbit determination, design, measurement, adjustment, and complete calculations for the position, tracking, and prediction of satellites and deep spacecraft. It emphasizes specific methods, related mathematical calculations, and worked examples and exercises. Therefore, technicians and engineers in the aerospace industry can directly apply them to their practical work. Dedicated to undergraduate students and graduate students, researchers, and professionals in astronomy, physics, space science, and related aerospace industries, the book is an integrated work based on the accumulated knowledge in satellite orbit dynamics and the author’s more than five decades of personal research and teaching experience in astronomy and aerospace dynamics.
Pindex Textbook 2023
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沙發(fā)
發(fā)表于 2025-3-21 23:05:45 | 只看該作者
板凳
發(fā)表于 2025-3-22 02:30:47 | 只看該作者
地板
發(fā)表于 2025-3-22 06:50:24 | 只看該作者
Lin LiuPresents basic theory, equations, and calculation of satellite orbits, for students.Provides calculations for design, tracking, prediction, and adjustment of satellite orbit or deep spacecrafts.Contai
5#
發(fā)表于 2025-3-22 09:56:37 | 只看該作者
6#
發(fā)表于 2025-3-22 12:53:55 | 只看該作者
https://doi.org/10.1007/978-3-662-34639-6The main content of orbital dynamics is about solving a dynamical problem.
7#
發(fā)表于 2025-3-22 17:56:00 | 只看該作者
https://doi.org/10.1007/978-3-662-34640-2The motions of satellites, including all sorts of spacecraft, in circling orbits correspond to perturbed dynamical systems.
8#
發(fā)表于 2025-3-22 23:32:59 | 只看該作者
https://doi.org/10.1007/978-3-663-09640-5To solve a dynamical problem, a mathematical model is required.
9#
發(fā)表于 2025-3-23 02:32:07 | 只看該作者
Der Volksgerichtshof und sein BeobachterIn the Introduction of this book, we describe that in the Solar System all motions of major planets and asteroids, and motions of natural and artificial satellites (such as Earth’s artificial satellites, the Moon’s satellites, Mars’s satellites, and other orbiting spacecraft) have only one main external force.
10#
發(fā)表于 2025-3-23 09:30:22 | 只看該作者
https://doi.org/10.1007/978-3-658-30299-3Generally speaking, orbital variations of a satellite are mainly due to the central body’s non-spherical gravity potential except for low orbit satellites with relatively large area-to-mass ratios (not including the low Moon orbit satellite because the Moon has no atmosphere).
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