Spacecraft Momentum Control Systems
暫譯: 太空船動量控制系統
Leve, Frederick a., Peck, Mason a., Hamilton, Brian J.
相關主題
商品描述
With space-industry professionals and university students, this book offers a practical technical reference for seeking to understand the state of the art in spacecraft momentum control systems. The focus is control moment gyroscope (CMG) technology, but general principles of momentum control--for example, through reaction wheels, magnetic torque actuation, and other means--are presented. These key topics are treated in several contexts: systems engineering and spacecraft architecture, attitude control and dynamics, and mission operations. The subject matter is developed with theoretical rigor and in terms of practical implementation in flight hardware software.
This book is the first to address CMG technology in depth, let alone from a practitioner's perspective. It is also timely, given the rise of commercial Earth imaging, the imminent need for high-torque manipulation of satellites for servicing and assembly, the advances in privately built spacecraft (including small satellites), and the growing popularity of the subject matter in academia over the past two decades. The current edition includes exercises suitable for upper-level undergraduate courses and graduate-level courses in spacecraft attitude dynamics and control, spacecraft design, and space systems engineering.
This second edition provides more applications, attitude control, momentum and nutation dumping, isolation, system identification, systems engineering, bearings, and structures as well as more in depth discussions of equations of motion, as well as the numerics and complexity associated with generalized inverses that are used for steering algorithms.
商品描述(中文翻譯)
本書針對太空產業專業人士和大學生，提供了一本實用的技術參考，旨在了解航天器動量控制系統的最新技術。重點在於控制力矩陀螺儀（Control Moment Gyroscope, CMG）技術，但也介紹了動量控制的一般原則，例如通過反應輪、磁力矩驅動和其他手段進行控制。這些關鍵主題在幾個背景下進行探討：系統工程和航天器架構、姿態控制和動力學，以及任務操作。該主題以理論嚴謹的方式發展，並考慮到在飛行硬體和軟體中的實際實施。
本書是第一本深入探討CMG技術的著作，更不用說是從實務者的角度來看。考慮到商業地球成像的興起、對衛星進行高扭矩操作以進行維護和組裝的迫切需求、私營公司建造的航天器（包括小型衛星）的進步，以及過去二十年來學術界對該主題日益增長的關注，這本書的出版時機恰到好處。本版包括適合高年級本科課程和研究生課程的練習，涵蓋航天器姿態動力學與控制、航天器設計和太空系統工程。
本書第二版提供了更多的應用、姿態控制、動量和進動耗散、隔離、系統識別、系統工程、軸承和結構，並對運動方程進行了更深入的討論，以及與用於引導算法的廣義逆矩陣相關的數值和複雜性。
作者簡介
Frederick A. Leve Program Officer at the Air Force Research Laboratory, Air Force Office of Scientific Research, received his Ph.D. in Aerospace Engineering from the University of Florida in 2010. While at the University of Florida, he received the IAF Silver Hermann Oberth Medal and the AIAA Abe Zarem Award for Astronautics. Currently, he runs a basic research program in dynamical systems and control theory and leads the Autonomy Working Group. He has published many papers in the area of attitude dynamics and control, specifically with respect to momentum control systems and also performs research in under-actuated control, fault tolerant control, control allocation, analytical mechanics, and system identification. Dr. Leve is a recipient of the 2014 AFRL Early Career Award.
Brian J. Hamilton Former Engineering Fellow at Honeywell Aerospace, received a BSEE with Honors from the University of Illinois, 1976. Mr. Hamilton has 42 years of experience at Honeywell (formerly, Sperry) and has participated in the development of CMG technology since its infancy. In later years, his research focus has been on CMG array control and steering, and the general application of momentum systems to agile spacecraft attitude control. Other areas of specialty include nonlinear modeling, controls design, system optimization and active magnetic suspension. Mr. Hamilton holds 12 patents.
Mason A. Peck Professor of Astronautics at Cornell University, received his Ph.D. in Aerospace Engineering from the University of California, Los Angeles, in 2001. He has worked as an aerospace engineer since 1994 and has been on the faculty at Cornell since 2004. From late 2011 through early 2014, he was NASA's Chief Technologist. In that role, he served as the agency's chief strategist for technology investment and prioritization and advocate for innovation in aeronautics and space technology. His research lab focuses on fundamental research in space technology that can be advanced through flight experiments. Examples include Violet, a nanosatellite for demonstrating CMG steering laws, and KickSat, the world's first crowdfunded spacecraft. Dr. Peck holds 19 patents in the USA and the E.U. and has over 100 academic publications. He received the NASA Distinguished Public Service Medal in 2014.
William Bialke Former Chief Engineer of Ithaco Space Systems, received a BSME with Honors from North Dakota State University in 1983. Mr Bialke has devoted his entire career to the development and manufacture of reaction wheels used on over 250 spacecraft, starting with Honeywell, and later as the architect of the Ithaco reaction wheel product line. He has written a number of papers on reaction wheel design tradeoffs, micro-vibration disturbance sources and bearing failure modes. He was lead investigator of a root cause analysis of on-orbit reaction wheel failures spanning 16 years, which led to a discovery of electrical discharge as the primary contributor to anomalies and failures in reaction wheel bearings. Mr. Bialke holds 6 patents.作者簡介(中文翻譯)
弗雷德里克·A·利夫 美國空軍研究實驗室科學研究辦公室的計畫官，於2010年在佛羅里達大學獲得航空工程博士學位。在佛羅里達大學期間，他獲得了IAF銀獎赫爾曼·奧伯斯獎和AIAA艾比·扎瑞姆航天獎。目前，他負責動態系統和控制理論的基礎研究計畫，並領導自主工作組。他在姿態動力學和控制領域發表了多篇論文，特別是在動量控制系統方面，並且還進行了欠驅動控制、容錯控制、控制分配、分析力學和系統識別的研究。利夫博士是2014年AFRL早期職業獎的獲得者。
布萊恩·J·漢密爾頓 前霍尼韋爾航空航天工程研究員，於1976年在伊利諾伊大學獲得榮譽電機工程學士學位。漢密爾頓先生在霍尼韋爾（前身為斯佩里）擁有42年的工作經驗，自CMG技術起步以來參與了其開發。在後期，他的研究重點是CMG陣列控制和引導，以及動量系統在靈活航天器姿態控制中的一般應用。其他專長領域包括非線性建模、控制設計、系統優化和主動磁懸浮。漢密爾頓先生擁有12項專利。
梅森·A·佩克 康奈爾大學航天學教授，於2001年在加州大學洛杉磯分校獲得航空工程博士學位。自1994年以來，他一直擔任航空工程師，自2004年以來在康奈爾大學任教。從2011年底到2014年初，他擔任NASA首席技術專家。在這個角色中，他擔任該機構技術投資和優先排序的首席策略師，並倡導航空和太空技術的創新。他的研究實驗室專注於可以通過飛行實驗推進的太空技術基礎研究。例子包括Violet，一個用於演示CMG引導法則的納米衛星，以及KickSat，世界上第一個眾籌的航天器。佩克博士在美國和歐盟擁有19項專利，並有超過100篇學術出版物。他於2014年獲得NASA傑出公共服務獎章。
威廉·比爾克 前伊薩科太空系統首席工程師，於1983年在北達科他州立大學獲得榮譽機械工程學士學位。比爾克先生將整個職業生涯奉獻於反應輪的開發和製造，這些反應輪被用於超過250個航天器，最初在霍尼韋爾工作，後來成為伊薩科反應輪產品線的架構師。他撰寫了多篇有關反應輪設計權衡、微振動擾動源和軸承故障模式的論文。他是針對16年來在軌反應輪故障的根本原因分析的首席調查員，這項研究發現電氣放電是反應輪軸承異常和故障的主要原因。比爾克先生擁有6項專利。
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