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Space Trajectories
◆JpGU2025 セール開催中！：2025年6月30日(月)ご注文分まで
※上記表示の販売価格は割引適用後の価格です 出版済み 3-5週間でお届けいたします。 Basic and Advanced Topics Author: Cerf, Max (ArianeGroup, France) Publisher: Wiley ISBN: 9781394293797 Cover: HARDCOVER Date: 2024年10月 こちらの商品は学校・法人様向け（機関契約）のオンラインブック版がございます。 オンラインブックの価格、納期につきましては弊社営業員または当ECサイトよりお問い合わせください。  DESCRIPTION An authoritative reference that covers essential concepts of orbital mechanics and explains how they relate to advanced space trajectory applications Space Trajectories is the first book to offer a comprehensive exploration of orbital mechanics and trajectory optimization in a single volume. Beginning with a review of essential concepts, the book progresses to advanced space applications, highlighting methods used in today’s space missions. The contents are organized into three parts. The first part delves into free orbital motion, covering topics such as Keplerian motion, perturbed motion, the three-body problem, orbit determination, and collision risks in orbit. The second part focuses on controlled orbital motion, discussing impulsive transfer, orbital rendezvous, thrust level optimization, low-thrust transfer, and space debris cleaning. The third part examines ascent and reentry, including launch into orbit, launcher staging, analytical solutions in flat Earth, interplanetary missions, and atmospheric reentry. Each chapter is written in a modular way, featuring conclusion summaries, key points, and suggestions for further investigation. Examples are included with detailed solutions methods that readers can apply to solve their own trajectory problems. Written by an expert of the topic who has performed guidance of Ariane launchers for 30 years, Space Trajectories includes information on: * Keplerian motion, motion time law, universal formulation, equinoctial parameters, and Lagrange coefficients * Osculating orbit, Gauss equations, gravitational and third body perturbations, Lissajous and Halo orbits, and invariant manifolds * Astrometry measurements, Kalman filtering, orbit uncertainties, and collision probability * Transfer in one, two, or three impulses, minimum-energy transfer, Lambert’s problem, high- and low-thrust transfer, and interplanetary path * Launch and reentry trajectories, propulsion systems, optimized thrust profiles, and launcher staging Space Trajectories is an essential reference for students and researchers aiming to quickly understand the main issues in astrodynamics and the way to design trajectories, as well as space engineers seeking to consolidate their knowledge in the field of optimization and optimal control applied to aerospace and space missions. TABLE OF CONTENTS Part I Free Orbital Motion 1 1 Two-Body Problem 3 2 Perturbed Motion 33 3 Three-Body Problem 67 4 Orbit Determination 95 5 Collision Risks 121 Part II Controlled Orbital Motion 147 6 Impulsive Transfer 149 7 Orbital Rendezvous 187 8 Optimal Thrust Level 215 9 Low-Thrust Transfer 239 10 Space Debris Cleaning 275 Part III Launch and Reentry 299 11 Launch into Orbit 301 12 Launcher Staging 329 13 Flat Earth Solutions 355 14 Interplanetary Trajectory 383 15 Atmospheric Reentry 411
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