Spacecraft Modeling, Attitude Determination, and Control: Quaternion-Based Approach, Second Edition
暫譯: 太空載具建模、姿態決定與控制：基於四元數的方法（第二版）
Yang, Yaguang
- 出版商: CRC
- 出版日期: 2026-10-16
- 售價: $2,690
- 貴賓價: 9.5 折 $2,555
- 語言: 英文
- 頁數: 394
- 裝訂: Quality Paper - also called trade paper
- ISBN: 1032954140
- ISBN-13: 9781032954141
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相關分類:
控制系統 Control-systems
尚未上市，無法訂購
相關主題
商品描述
This book discusses spacecraft attitude control-related topics: spacecraft modeling, spacecraft attitude determination and estimation, and spacecraft attitude controls. Unlike other books addressing these topics, this book focuses on quaternion-based methods because of their many merits. It provides a brief but necessary background on rotation sequence representations and frequently used reference frames that form the foundation of spacecraft attitude description. It then discusses the fundamentals of attitude determination using vector measurements, various efficient (including very recently developed) attitude determination algorithms, and the instruments and methods of popular vector measurements. With available attitude measurements, attitude control designs for inertial point and nadir pointing are presented in terms of required torques which are independent of actuators in use. Given the required control torques, some actuators are not able to generate the accurate control torques; therefore, spacecraft attitude control design methods with achievable torques for these actuators (for example, magnetic torque bars and control moment gyros) are provided. Some rigorous controllability results are provided.
The book also includes attitude control in some special maneuvers and systems, such as orbital-raising, docking and rendezvous, and multi-body space systems that are normally not discussed in similar books. All design methods are based on state-spaced modern control approaches, such as linear quadratic optimal control, robust pole assignment control, model predictive control, and gain scheduling control. Applications of these methods to spacecraft attitude control problems are provided. Appendices are provided for readers who are not familiar with these topics.
商品描述(中文翻譯)
本書探討太空船姿態控制相關主題，包括太空船建模、太空船姿態決定與估測，以及太空船姿態控制。不同於其他探討這些主題的書籍，本書著重於以四元數為基礎的方法，因為這類方法具有許多優點。書中簡要介紹旋轉序列表示法，以及構成太空船姿態描述基礎、經常使用的參考座標系。接著，本書探討使用向量測量進行姿態決定的基本原理、各種高效率的姿態決定演算法（包括近期開發的演算法），以及常見向量測量所使用的儀器與方法。
利用可取得的姿態測量值，本書以所需力矩的形式介紹慣性指向與天底指向的姿態控制設計，而這些所需力矩與所使用的致動器無關。由於某些致動器無法產生精確的控制力矩，因此，針對這些致動器（例如磁力矩桿與控制力矩陀螺儀），本書也提供以可實現力矩為基礎的太空船姿態控制設計方法。此外，書中亦提供若干嚴謹的可控性結果。
本書還涵蓋一些在類似書籍中通常未被討論的特殊機動與系統中的姿態控制，例如軌道提升、對接與交會，以及多體太空系統。所有設計方法皆以狀態空間現代控制方法為基礎，例如線性二次最佳控制、強健極點配置控制、模型預測控制，以及增益排程控制。書中並提供這些方法應用於太空船姿態控制問題的實例。對於不熟悉相關主題的讀者，書末附有必要的附錄。
作者簡介
Yaguang Yang holds B.S. (1982) and M.S. (1985) degrees from Huazhong University of Science and Technology, China. From 1985 to 1990, he was a lecturer at Zhejiang University in China. In 1996 he received a PhD degree from the Department of Electrical and Computer Engineering at the University of Maryland, College Park, Maryland, USA. Since then, he has designed and implemented control systems at UKIRT, CIENA, ITT, and Orbital Sciences Corporation; he has performed theoretical and applied research and published more than 50 papers in controls and optimizations, developed and implemented algorithms in computer codes, and applied to engineering problems, and he has managed nuclear power plant instrument and control research projects at US NRC. He is currently a system engineer with the Goddard Space Flight Center, NASA, where he has worked on several space projects, including The Laser Interferometer Space Antenna (LISA), Enceladus Life Signatures and Habitability (ELSAH), The Large UV/Optical/IR Surveyor (LUVOIR), and is the Principal Investigator (PI) of an applied research project (Model-based optimal engineering design and its application to the advanced trajectory design problem).
作者簡介(中文翻譯)
Yaguang Yang 於 1982 年取得中國華中科技大學學士學位，並於 1985 年取得碩士學位。1985 年至 1990 年間，他擔任中國浙江大學講師。1996 年，他取得美國馬里蘭州 College Park 的 University of Maryland 電機與電腦工程系博士學位。此後，他曾在 UKIRT、CIENA、ITT 及 Orbital Sciences Corporation 設計與實作控制系統；從事理論與應用研究，在控制與最佳化領域發表超過 50 篇論文；開發並實作電腦程式中的演算法，並將其應用於工程問題；此外，他也曾在 US NRC 管理核電廠儀器與控制研究計畫。
目前，他任職於 NASA 的 Goddard Space Flight Center，擔任系統工程師，參與多項太空計畫，包括 The Laser Interferometer Space Antenna（LISA）、Enceladus Life Signatures and Habitability（ELSAH）及 The Large UV/Optical/IR Surveyor（LUVOIR）。此外，他也是一項應用研究計畫「以模型為基礎的最佳化工程設計及其在進階軌跡設計問題上的應用」（Model-based optimal engineering design and its application to the advanced trajectory design problem）的首席研究員（Principal Investigator，PI）。
