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001453082 001__ 1453082
001453082 003__ OCoLC
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001453082 020__ $$a9783031047800$$q(electronic bk.)
001453082 020__ $$a303104780X$$q(electronic bk.)
001453082 020__ $$z3031047796
001453082 020__ $$z9783031047794
001453082 0247_ $$a10.1007/978-3-031-04780-0$$2doi
001453082 035__ $$aSP(OCoLC)1347430706
001453082 040__ $$aYDX$$beng$$cYDX$$dGW5XE$$dOCLCF
001453082 049__ $$aISEA
001453082 050_4 $$aTL3250
001453082 08204 $$a629.4742$$223/eng/20221021
001453082 1001_ $$aFichter, Walter,$$eauthor.
001453082 24510 $$aPrinciples of spacecraft control :$$bconcepts and theory for practical applications /$$cWalter Fichter, Ramin T. Geshnizjani.
001453082 260__ $$aCham, Switzerland :$$bSpringer,$$c[2023].
001453082 300__ $$a1 online resource
001453082 504__ $$aIncludes bibliographical references and index.
001453082 5050_ $$aSystem Engineering Basics -- Satellite Motion Models -- Rotational State Determination -- Actuator Commanding -- Attitude and Momentum Control -- Accelerometers and Drag-Free Control -- Closing Remarks.
001453082 506__ $$aAccess limited to authorized users.
001453082 520__ $$aThe objective of this textbook is to provide the mathematical models and algorithms needed to develop a thorough understanding of all control system functions of a rigid body spacecraft. Relatively simple, but practically applicable algorithms are presented rather than recent advances. We try to avoid detailed and specialized issues that are of less importance for the fundamental understanding, such as detailed environment models, etc. Furthermore, control problems that can be cast in standard formulations and solved with existing methods are not treated here. Instead, we intend to provide an understanding of the principles, put them in an engineering context, and try to give all explanations as concise as possible. Besides conventional three-axis attitude control systems, the following topics are treated in this book: Control of agile rotation maneuvers using control moment gyros Precise pointing control with error classes for pointing instruments Control systems with accelerometers and free-flying test masses, which provide low-disturbance or disturbance-free environments We believe that these topics are of considerable relevance for the design of future spacecraft control systems, especially in the field of science and Earth observation missions. The Authors Walter Fichter has been in industry for many years, working in the field of guidance, navigation, and controls for spacecraft. Since 2007 he is professor of flight mechanics and controls at the University of Stuttgart. His current research interests include autonomy of aerospace vehicles, intelligent flight, guidance and control of UAVs and urban air mobility vehicles. Ramin Geshnizjani was a researcher at the Institute of Flight Mechanics and Controls of the University of Stuttgart and now works as a development engineer in the aerospace industry. His research interests and current activities include attitude control of agile spacecraft with control moment gyros, navigation and state estimation, and pointing control.
001453082 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed October 21, 2022).
001453082 650_0 $$aSpace vehicles$$xControl systems.
001453082 655_0 $$aElectronic books.
001453082 7001_ $$aGeshnizjani, Ramin T.$$eauthor.
001453082 77608 $$iPrint version: $$z3031047796$$z9783031047794$$w(OCoLC)1305914866
001453082 852__ $$bebk
001453082 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-3-031-04780-0$$zOnline Access$$91397441.1
001453082 909CO $$ooai:library.usi.edu:1453082$$pGLOBAL_SET
001453082 980__ $$aBIB
001453082 980__ $$aEBOOK
001453082 982__ $$aEbook
001453082 983__ $$aOnline
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