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Titlebook: Low Energy Flight: Orbital Dynamics and Mission Trajectory Design; Jianping Yuan,Yu Cheng,Chong Sun Book 2019 Science Press and Springer N

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發(fā)表于 2025-3-21 19:57:42 | 只看該作者 |倒序瀏覽 |閱讀模式
書目名稱Low Energy Flight: Orbital Dynamics and Mission Trajectory Design
編輯Jianping Yuan,Yu Cheng,Chong Sun
視頻videohttp://file.papertrans.cn/589/588768/588768.mp4
概述Provides an analytical approach for continuous low-thrust trajectory design.Presents a general, two-maneuver transfer procedure from a libration point orbit in the Earth–Moon system to a lunar orbit.O
圖書封面Titlebook: Low Energy Flight: Orbital Dynamics and Mission Trajectory Design;  Jianping Yuan,Yu Cheng,Chong Sun Book 2019 Science Press and Springer N
描述The book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving classical problems or address emerging problems that have yet to be studied, including low-thrust transfer trajectory design using the virtual gravity field method; transfer in the three-body system using invariant manifolds; formation flying under space-borne artificial magnetic fields; and the orbital dynamics of highly irregular asteroids. It also features an extensive study of the orbital dynamics in the vicinity of contact binary asteroids, including the 1:1 ground-track resonance, the equilibrium points and their stability, and the third-order analytical solution of orbital motion in the vicinity of the non-collinear equilibrium point..?.Given its breadth of coverage, the book offers a valuable reference guide for allengineers and researchers interested in the potential applications of low-energy space missions..?.
出版日期Book 2019
關(guān)鍵詞Low-energy flight; Orbital dynamics; Mission trajectory design; Low-thrust; Formation flying; Contact bin
版次1
doihttps://doi.org/10.1007/978-981-13-6130-2
isbn_ebook978-981-13-6130-2
copyrightScience Press and Springer Nature Singapore Pte Ltd. 2019
The information of publication is updating

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Introduction,hest from Earth is the Voyager 1 spacecraft (NASA), which obtained images of Saturn and Jupiter during their flybys. Currently, it has arrived at the outer solar system, i.e. the edge of the solar influence and interstellar medium.
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Transfer Between Libration Point Orbits and Lunar Orbits in Earth-Moon System, . point (of several amplitudes) and lunar polar orbits with altitudes varying between 100 and 500?km, the procedure we develop can be applied to any kind of lunar orbits, libration orbits around the . or . points of the Earth-Moon system, or to other similar cases with different values of the mass ratio.
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tion point orbit in the Earth–Moon system to a lunar orbit.OThe book focuses on the orbital dynamics and mission trajectory (transfer or target trajectory) design of low-energy flight in the context of modern astrodynamics. It investigates various topics that either offer new methods for solving cla
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