| 书目名称 | Low Energy Flight: Orbital Dynamics and Mission Trajectory Design | | 编辑 | Jianping Yuan,Yu Cheng,Chong Sun | | 视频video | | | 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 | | 图书封面 |  | | 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 | | 关键词 | Low-energy flight; Orbital dynamics; Mission trajectory design; Low-thrust; Formation flying; Contact bin | | 版次 | 1 | | doi | https://doi.org/10.1007/978-981-13-6130-2 | | isbn_ebook | 978-981-13-6130-2 | | copyright | Science Press and Springer Nature Singapore Pte Ltd. 2019 |
The information of publication is updating
|
|
发表于 2025-3-21 19:57:42
