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Titlebook: Orbital Relative Motion and Terminal Rendezvous; Analytic and Numeric Jean Albert Kéchichian Book 2021 The Editor(s) (if applicable) and Th

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发表于 2025-3-21 19:37:32 | 显示全部楼层 |阅读模式
书目名称Orbital Relative Motion and Terminal Rendezvous
副标题Analytic and Numeric
编辑Jean Albert Kéchichian
视频video
概述Addresses the problem of terminal rendezvous in Earth orbit subjected to perturbations.Equations can be coded by users to develop flight software.Provides detailed mathematical derivations and actual
丛书名称Space Technology Library
图书封面Titlebook: Orbital Relative Motion and Terminal Rendezvous; Analytic and Numeric Jean Albert Kéchichian Book 2021 The Editor(s) (if applicable) and Th
描述This book provides a comprehensive analysis of time-fixed terminal rendezvous around the Earth using chemical propulsion..The book has two main objectives. The first is to derive the mathematics of relative motion in near-circular orbit when subjected to perturbations emanating from the oblateness of the Earth, third-body gravity, and atmospheric drag. The mathematics are suitable for quick trajectory prediction and the creation of computer codes and efficient software to solve impulsive maneuvers and fly rendezvous missions..The second objective of this book is to show how the relative motion theory is applied to the exact precision-integrated, long-duration, time-fixed terminal rendezvous problem around the oblate Earth for the general elliptic orbit case..The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics,and students at the graduate level and above. .
出版日期Book 2021
关键词orbital mechanics; spacecraft guidance; space vehicle interception; orbital rendezvous; rendezvous in ea
版次1
doihttps://doi.org/10.1007/978-3-030-64657-8
isbn_softcover978-3-030-64659-2
isbn_ebook978-3-030-64657-8Series ISSN 0924-4263 Series E-ISSN 2542-8896
issn_series 0924-4263
copyrightThe Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl
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The Second-Order Analytic Approximation to the Solution of the Euler-Hill Equations of Relative Motfrom the origin of the frame, it is felt that because of the presence of initial non-zero velocities, the subsequent motion may drift to considerable distances from the origin of the frame, thereby, degrading the accuracy of the analytic first-order solution of the equations of motion. The initial v
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The Analysis and Implementation of In-Plane Stationkeeping of Continuously Perturbed Walker Constelgiven tolerance deadband is about to be violated. This chapter illustrates the computations associated with the stationkeeping of a generic Walker constellation, by maneuvering each leading spacecraft within an orbit plane, and calculating the associated velocity changes required for controlling the
发表于 2025-3-22 09:51:36 | 显示全部楼层
Book 2021liptic orbit case..The contents are both theoretical and applied, with long-lasting value for aerospace engineers, trajectory designers, professors of orbital mechanics,and students at the graduate level and above. .
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Space Technology Libraryhttp://image.papertrans.cn/o/image/703594.jpg
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Analytic Solutions for the Perturbed Motion of a Spacecraft in Near-Circular Orbit, Under the Influturbed by Earth’s . and . zonals, and described in the rotating Euler-Hill frame, the same approach is used in this chapter and based on Reference [2] to obtain analytic expression for the spacecraft motion perturbed by the luni-solar gravity.
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The Mathematical Models of the Jet Propulsion Laboratory (JPL) Artificial Satellite Analysis PrograThis chapter shows the equations used in the JPL computer program ASAP that are specific to the modeling of the central body disturbing function, the third-body disturbing function, as well as the equations of motion due to atmospheric drag. These descriptions are taken directly from Reference [1] by Kwok.
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