{"title":"Chen Yang","description":"\u003cp\u003e\u0026lt;p\u0026gt;Chen Yang is an associate professor at Beihang University. He received his B.S., M.S., and Ph.D. degrees from Beihang University, Beijing, China, and his main research interests are spacecraft attitude\/vibration control, uncertainty-oriented control system, and reliability-based design optimization of control system. He has won Marie Skłodowska-Curie Actions (MSCA) Fellowships. He has been awarded \"whole career\" and \"single year\" in the World's Top 2% Scientists list published by Stanford University and the Elsevier database. He has published more than 100 papers, including more than 60 SCI papers as first or corresponding author, and 1 monograph as the first author. He has presided over more than 20 projects, including the National Natural Science Foundation of China, etc.\u0026lt;\/p\u0026gt;\u003cbr\u003e\u0026lt;p\u0026gt;Yuanqing Xia is an IEEE fellow and received the grant from the National Science Foundation for Distinguished Young Scholars of China and the Cheung Kong Scholars Programme of China. He has been awarded \"Highly Cited Chinese Researchers\" published by the Elsevier database. He received the Ph.D. degree in control theory and control engineering from Beihang University, Beijing, China, in 2001. He was a research fellow in several academic institutions from 2002 to 2008, including the National University of Singapore and the University of Glamorgan, UK. Since 2004, he has been with the Beijing Institute of Technology, China, where he is currently a full professor.\u0026lt;\/p\u0026gt;\u003cbr\u003e\u0026lt;p\u0026gt;\u0026amp;nbsp;\u0026lt;\/p\u0026gt;\u003cbr\u003e\u0026lt;p\u0026gt;Yuanqing Xia is an IEEE Fellow and received the grant from the National Science Foundation for Distinguished Young Scholars of China and the Cheung Kong Scholars Programme of China. He has been awarded \"Highly Cited Chinese Researchers\" published by the Elsevier database. He received the Ph.D. degree in control theory and control engineering from Beihang University, Beijing, China, in 2001. He was a Research Fellow in several academic institutions from 2002 to 2008, including the National University of Singapore and the University of Glamorgan, U.K. Since 2004, he has been with the Beijing Institute of Technology, China, where he is currently a Full Professor. His research interests include flight control, cloud control systems for flight, networked control systems, robust control and signal processing, and active disturbance rejection control. He is the Director of the specialized committee on cloud control and decision of the Chinese Institute of Command and Control (CICC), a member of the 8th Disciplinary Review Group of the Academic Degrees Committee of the State Council, a member of the Big Data Expert Committee of the Chinese Computer Society, and the Vice Chairperson of the Internet of Things Working Committee of the Chinese Institute of Instrumentation. He is a Deputy Editor of the Journal of Beijing Institute of Technology, an Associate Editor of Acta Automatica Sinica, International Journal of Automation and Computing, Gyroscopy and Navigation, and IET Control Theory and Applications.\u0026lt;\/p\u0026gt;\u003c\/p\u003e","products":[{"product_id":"set-theory-based-spacecraft-dynamics-and-control-chen-yang-ebook","title":"Set Theory-Based Spacecraft Dynamics and Control","description":"\u003cp\u003eIntroduction.- Interval-oriented Reduced-order Model for Uncertain Systems.- Convex Model-based Reduced-order Model for Uncertain Control Systems.- Uncertain robust attitude determination based on set theory.- Uncertain optimal attitude control for space power satellite based on interval Riccati equation with non-probabilistic time-dependent reliability.- Uncertain iterative optimal attitude control method for periodic satellite with reliability constraint.- Reliability-constrained uncertain spacecraft sliding mode attitude control with set theory.- Reliability-constrained optimal attitude-vibration control for rigid-flexible coupling satellite using interval dimension-wise analysis.- Bounded model predictive control for rigid-flexible coupling satellite with reliability constraint.- Hybrid-uncertainty-based attitude control for rigid-flexible satellite considering degradation and non-probabilistic reliability.\u003c\/p\u003e","brand":"Chen Yang","offers":[{"title":"Default Title","offer_id":53939291029831,"sku":"9789819591794","price":181.89,"currency_code":"EUR","in_stock":true}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0920\/5455\/2903\/files\/set-theory-based-spacecraft-dynamics-and-control-ebook-cover.webp?v=1779127380"}],"thumbnail_url":"\/\/cdn.shopify.com\/s\/files\/1\/0920\/5455\/2903\/collections\/chen-yang-autor-kollektion.webp?v=1779127377","url":"https:\/\/www.cinebuch.de\/collections\/chen-yang.oembed","provider":"CineBuch","version":"1.0","type":"link"}