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標(biāo)題: Titlebook: Algorithms for Satellite Orbital Dynamics; Lin Liu Textbook 2023 Nanjing University Press 2023 Orbit elements.Orbit determination.Satellit [打印本頁(yè)]

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作者: Lipoprotein(A)    時(shí)間: 2025-3-21 23:05

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作者: syncope    時(shí)間: 2025-3-22 06:50
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
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作者: certitude    時(shí)間: 2025-3-22 12:53
https://doi.org/10.1007/978-3-662-34639-6The main content of orbital dynamics is about solving a dynamical problem.
作者: myocardium    時(shí)間: 2025-3-22 17:56
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.
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https://doi.org/10.1007/978-3-663-09640-5To solve a dynamical problem, a mathematical model is required.
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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.
作者: 植物茂盛    時(shí)間: 2025-3-23 09:30
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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作者: 珍奇    時(shí)間: 2025-3-23 14:35
https://doi.org/10.1007/978-3-662-65690-7As given in previous chapters that the differential equations, which describe the motions of celestial bodies and spacecraft in the Solar System, are extremely complicated.
作者: RAG    時(shí)間: 2025-3-23 21:39
Das Arbeiten mit den Vorrichtungen,The orbit determination can be directly defined as the process of determining the motion state of an orbit of a celestial body (including various spacecraft) at a given time . from a certain number of tracking measurements using proper mathematical methods.
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Selections and Transformations of Coordinate Systems,The main content of orbital dynamics is about solving a dynamical problem.
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The Complete Solution for the Two-Body Problem,The motions of satellites, including all sorts of spacecraft, in circling orbits correspond to perturbed dynamical systems.
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作者: SLING    時(shí)間: 2025-3-24 15:26
,Analytical Non-singularity Perturbation Solutions for Extrapolation of Earth’s Satellite Orbital MoIn 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.
作者: 重畫(huà)只能放棄    時(shí)間: 2025-3-24 21:36

作者: 配偶    時(shí)間: 2025-3-25 02:59
Orbital Solutions of Satellites of the Moon, Mars, and Venus,In this section, we use three major planets, Earth, Mars, Venus, and the Moon as examples to show the characteristics.
作者: 壓碎    時(shí)間: 2025-3-25 06:49
Numerical Method for Satellite Orbit Extrapolations,As given in previous chapters that the differential equations, which describe the motions of celestial bodies and spacecraft in the Solar System, are extremely complicated.
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Precise Orbit Determination,In Sect.?., there is a simple definition of precise orbit determination compared to the initial orbit determination.
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作者: 沐浴    時(shí)間: 2025-3-25 20:25
2731-734X in satellite orbit dynamics and the author’s more than five decades of personal research and teaching experience in astronomy and aerospace dynamics.978-981-19-4841-1978-981-19-4839-8Series ISSN 2731-734X Series E-ISSN 2731-7358
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