Satellite Equivalence Orbits: Analysis of Orbits Combining Different Motions
暫譯: 衛星等效軌道：不同運動結合的軌道分析

Name: Satellite Equivalence Orbits: Analysis of Orbits Combining Different Motions
Price: 7477 TWD
Availability: OnlineOnly
Author: Jochim, Ernst Friedrich Maria
ISBN: 3031584759

Jochim, Ernst Friedrich Maria

出版商: Springer
出版日期: 2024-12-05
售價: $7,870
貴賓價: 9.5 折 $7,477
語言: 英文
頁數: 481
裝訂: Hardcover - also called cloth, retail trade, or trade
ISBN: 3031584759
ISBN-13: 9783031584756
相關分類: 衛星通訊 Satellite-networking

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商品描述

This book presents the essential characteristics of the different satellite motions. Satellite motions can be classified as anomalistic, draconitic, tropical, Hansen-, Kepler-, meridional, Sun-synodical, Moon-synodical motion, depending on the relevant reference point. When two of these types of motions (in some cases even more than two) are coupled, satellite orbits are obtained, which are called equivalence orbits in this book. They share the special properties of the different coupled motions and are therefore of particular interest in the selection of special satellite orbits.

In the book the author calculates mean equivalence orbits with secular perturbation formulas, as well as true equivalence orbits considering a complete orbit model including periodic motion effects. Some of the equivalence orbits can be determined unambiguously and with extremely high accuracy, they are stable in the long term. Others can only be found with low accuracy and reduced stability. The author investigates all possible combinations and the associated general equations of condition are derived in each case. Some well-known families of satellite orbits, such as the Sun-synchronous orbits, can be interpreted as mean equivalence orbits. The study of their stability is of great interest in orbit mechanics. Special applications and numerous numerical examples, graphical representations of all possible ranges of the Kepler elements, and detailed studies of the stability of particularly important equivalence orbits are carried out using the Brouwer orbit model as well as the modification by Eckstein.

This lays the foundation for possible refinements using arbitrary extended orbital models and for possibly required orbital corrections. Numerous problems are to deepen the treated topics and/or to stimulate for further investigations.

The book will be of interest to Astrodynamics and Aerospace Engineers as well as graduate students studying satellite orbits.

商品描述(中文翻譯)

本書介紹了不同衛星運動的基本特徵。衛星運動可以根據相關參考點分類為異常運動（anomalistic）、龍運動（draconitic）、熱帶運動（tropical）、漢森運動（Hansen）、開普勒運動（Kepler）、經度運動（meridional）、太陽同步運動（Sun-synodical）和月亮同步運動（Moon-synodical）。當這些運動類型中的兩種（在某些情況下甚至更多）相互耦合時，便會產生衛星軌道，這在本書中稱為等效軌道（equivalence orbits）。它們共享不同耦合運動的特殊性質，因此在選擇特殊衛星軌道時特別重要。

在本書中，作者使用長期擾動公式計算平均等效軌道，並考慮包括周期運動效應的完整軌道模型來計算真實等效軌道。一些等效軌道可以明確且極高精度地確定，並且在長期內是穩定的。其他的則只能以低精度和降低的穩定性來找到。作者研究所有可能的組合，並在每種情況下推導出相關的一般條件方程。一些著名的衛星軌道家族，如太陽同步軌道，可以被解釋為平均等效軌道。研究它們的穩定性在軌道力學中具有重要意義。使用布勞威（Brouwer）軌道模型以及艾克斯坦（Eckstein）的修改，進行了特殊應用和大量數值範例、開普勒元素所有可能範圍的圖形表示，以及對特別重要的等效軌道穩定性的詳細研究。

這為使用任意擴展軌道模型進行可能的細化和可能需要的軌道修正奠定了基礎。許多問題旨在深化所處理的主題和/或激發進一步的研究。

本書將對航天動力學和航空航天工程師以及研究衛星軌道的研究生感興趣。

作者簡介

Fritz Jochim holds a Diploma Degree (Master Degree) in mathematics and mathematical astronomy from University Würzburg, and got a Second State Degree for mathematics and physics as high school teacher in 1970. From 1970 - 2006 he worked a scientific employee at German Aerospace Center in Braunschweig and Oberpfaffenhofen. His main topic was satellite orbit analysis, development of a comprehensive package of analytical satellite orbit analysis programs, which are successfully used in almost all German satellite missions and space studies. He participated in studies like Helios, Symphonie, Erdsat, POLO (Polar Orbiting Lunar Observatory), Planetenteleskop, ENVISAT, AMPTE, CHAMP, ERS1/2, GRACE, Mars Express, Asteroid-Mission to minor planets, ROSAT, X-SAR (support of two shuttle missions in the POCC, Houston, USA), TerraSAR-X, TanDEM-X, TanDEM-L.

In 2011 he was awarded a Doctor Degree (Dr. Ing.) from UniBw München.

作者簡介(中文翻譯)

弗里茨·約希姆（Fritz Jochim）擁有維爾茨堡大學（University Würzburg）的數學及數學天文學碩士學位，並於1970年獲得數學和物理的第二國家教師資格證書。他於1970年至2006年在德國航空航天中心（German Aerospace Center）布倫瑞克（Braunschweig）和奧伯法芬霍芬（Oberpfaffenhofen）擔任科學員工，主要研究主題為衛星軌道分析，開發了一套全面的分析衛星軌道分析程式包，這些程式在幾乎所有德國的衛星任務和太空研究中都得到了成功應用。他參與了多個研究項目，如赫利奧斯（Helios）、交響曲（Symphonie）、地球衛星（Erdsat）、極軌月球觀測站（POLO）、行星望遠鏡（Planetenteleskop）、環境衛星（ENVISAT）、AMPTE、CHAMP、ERS1/2、GRACE、火星快車（Mars Express）、小行星任務（Asteroid-Mission to minor planets）、ROSAT、X-SAR（支持兩次在美國休士頓的航天飛行任務POCC）、TerraSAR-X、TanDEM-X、TanDEM-L。

2011年，他獲得慕尼黑國防軍大學（UniBw München）的博士學位（Dr. Ing.）。