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Principles of spacecraft controlconcepts and theory for practical applications /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Principles of spacecraft controlby Walter Fichter, Ramin T. Geshnizjani.
其他題名:	concepts and theory for practical applications /
作者:	Fichter, Walter.
其他作者:	Geshnizjani, Ramin T.
出版者:	Cham :Springer International Publishing :2023.
面頁冊數:	xvii, 193 p. :ill., digital ;24 cm.
Contained By:	Springer Nature eBook
標題:	Space vehiclesControl systems.
電子資源:	https://doi.org/10.1007/978-3-031-04780-0
ISBN:	9783031047800$q(electronic bk.)

Principles of spacecraft controlconcepts and theory for practical applications /
Fichter, Walter.

Principles of spacecraft controlconcepts and theory for practical applications /[electronic resource] :by Walter Fichter, Ramin T. Geshnizjani. - Cham :Springer International Publishing :2023. - xvii, 193 p. :ill., digital ;24 cm.

System Engineering Basics -- Satellite Motion Models -- Rotational State Determination -- Actuator Commanding -- Attitude and Momentum Control -- Accelerometers and Drag-Free Control -- Closing Remarks.

The 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.

ISBN: 9783031047800$q(electronic bk.)

Standard No.: 10.1007/978-3-031-04780-0doiSubjects--Topical Terms:

357231
Space vehicles
--Control systems.

LC Class. No.: TL3250

Dewey Class. No.: 629.4742

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