Advanced Attitude Control of Satellite: A Modeling Error Compensation Approach
暫譯: 衛星的高級姿態控制：一種建模誤差補償方法
Xiao, Bing, Chen, Zhaoyue, Xu, Jingwen
相關主題
商品描述
This book focuses on the high-accuracy attitude control system design and approaches for satellite with modeling error including system uncertainties, actuator faults, and disturbances. It presents a systematically and almost self-contained description of the many facets of envisaging, designing, implementing, or experimentally exploring modeling error compensation-based attitude control of satellites. The advanced treatment of practical issues in satellite attitude compensation control is one of the major features of the book, which is particularly suited for readers who are interested to learn the latest solutions in attitude control system design of satellites. The book intends to provide a unified platform for understanding and applicability of the modeling error compensation-based attitude control for different purposes in aerospace engineering and some related fields. It can benefit researchers, engineers, and graduate students in the fields of attitude control of satellites and other unmanned systems, aerospace engineering, etc.
商品描述(中文翻譯)
本書專注於高精度姿態控制系統的設計與方法，針對包含系統不確定性、驅動器故障及擾動的建模誤差進行探討。它系統性且幾乎自成一體地描述了設想、設計、實施或實驗探索基於建模誤差補償的衛星姿態控制的多個面向。本書的一大特色是對衛星姿態補償控制中實際問題的深入探討，特別適合對衛星姿態控制系統設計最新解決方案感興趣的讀者。本書旨在提供一個統一的平台，以便於理解和應用基於建模誤差補償的姿態控制，適用於航空航天工程及相關領域的不同目的。它將惠及衛星及其他無人系統的姿態控制、航空航天工程等領域的研究人員、工程師和研究生。
作者簡介
Dr. Xiao received the B.S. degree in mathematics from Tianjin Polytechnic University, Tianjin, China, in 2007, and the M.S. and Ph.D. degrees in control science and engineering from Harbin Institute of Technology, Harbin, China, in 2010 and 2014, respectively. From 2013 to 2014, he was a visiting scholar with the Department of Mechanical Engineering, Georgia Institute of Technology, USA. Between May 2014 and August 2017, he was a professor with the College of Engineering, Bohai University, China. From September 2018 to October 2021, he was an associate professor with the School of Automation, Northwestern Polytechnical University. Since November 2021, he has been the Professor of that university. His research interests include spacecraft attitude control and its fault-tolerant control design.
Dr. Chen received the B.S. and the Ph.D. degree in aeronautical and astronautical science and technology from Beijing Institute of Technology, Beijing, China, in 2014 and 2021, respectively. From 2018 to 2019, he was a visiting Ph.D. student with KU Leuven, Leuven, Belgium. From March 2023 to February 2024, he was a postdoctoral researcher with the Institute of Advanced Structure Technology, Beijing Institute of Technology. Since March 2024, he has been with the Beihang University, where he is currently an associate professor. His research interests include the dynamics of spacecraft, the structural dynamics, the advanced structure design, and their application to spacecraft.
Jingwen Xu received the B.S. and the M.S. degrees in computer science from Xi'an Jiaotong University, Xi'an, China, in 2013 and 2018, respectively. From 2018 to 2023, she worked as an engineer of the tracking and telecommand system of satellite in China Xi'an Satellite Control Center. From October 2023, she has been with the Northwestern Polytechnical University, where she is currently as an assistant research fellow. Her research interests include fault diagnosis and fault tolerant-control of satellite, attitude control engineering of satellite, and state estimation of satellite control system.
Dr. Cao received the B.S., the M.S., and the Ph.D. degrees in navigation, guidance, and control of spacecraft from the National University of Defense Technology, Changsha, China, in 2007, 2010, and 2014, respectively. From 2013 to 2014, he was a visiting Ph.D. student with the Department of Mechanical Engineering, McGill University, Canada. From 2014 to 2017, he was a senior engineer of the State Key Laboratory of Astronautic Dynamics, China Xi'an Satellite Control Center, China. Since 2018, he has been a research fellow with the National Innovation Institute of Defense Technology, Beijing, China. He has more than fifteen years' engineering experience in nanosatellite and designed attitude determination and control systems for eight in-orbital micro/nano satellites. His research interests include the areas of satellite navigation, control and dynamics, and state estimation.
作者簡介(中文翻譯)
蕭博士於2007年獲得中國天津理工大學數學學士學位，並於2010年和2014年分別獲得中國哈爾濱工業大學控制科學與工程碩士及博士學位。2013年至2014年，他曾擔任美國喬治亞理工學院機械工程系的訪問學者。2014年5月至2017年8月，他在中國渤海大學工程學院擔任教授。2018年9月至2021年10月，他在西北工業大學自動化學院擔任副教授。自2021年11月以來，他一直是該大學的教授。他的研究興趣包括航天器姿態控制及其容錯控制設計。
陳博士於2014年和2021年分別獲得中國北京理工大學航空航天科學與技術學士及博士學位。2018年至2019年，他曾在比利時魯汀大學擔任訪問博士生。2023年3月至2024年2月，他在北京理工大學先進結構技術研究所擔任博士後研究員。自2024年3月以來，他在北京航空航天大學任職，目前擔任副教授。他的研究興趣包括航天器的動力學、結構動力學、先進結構設計及其在航天器上的應用。
徐靜雯於2013年和2018年分別獲得中國西安交通大學計算機科學學士及碩士學位。2018年至2023年，她在中國西安衛星測控中心擔任衛星跟蹤與遙控系統工程師。自2023年10月以來，她在西北工業大學任職，目前擔任助理研究員。她的研究興趣包括衛星的故障診斷與容錯控制、衛星的姿態控制工程及衛星控制系統的狀態估計。
曹博士於2007年、2010年和2014年分別獲得中國國防科技大學航天器導航、引導與控制學士、碩士及博士學位。2013年至2014年，他曾在加拿大麥吉爾大學機械工程系擔任訪問博士生。2014年至2017年，他在中國西安衛星測控中心的航天動力學國家重點實驗室擔任高級工程師。自2018年以來，他在北京的國防科技創新研究院擔任研究員。他在微衛星的工程經驗超過十五年，並為八顆在軌微/納衛星設計了姿態確定與控制系統。他的研究興趣包括衛星導航、控制與動力學及狀態估計等領域。
