Principles of Spacecraft Control

Walter Fichter

ISBN 10: 3031047796 / ISBN 13: 9783031047794

Published by Springer, Palgrave Macmillan Okt 2022, 2022

About this Item

This item is printed on demand - Print on Demand Titel. Neuware -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.Springer-Verlag KG, Sachsenplatz 4-6, 1201 Wien 212 pp. Englisch.

Seller Inventory # 9783031047794

Bibliographic Details

• Title: Principles of Spacecraft Control
• Publisher: Springer, Palgrave Macmillan Okt 2022
• Publication Date: 2022
• Language: English
• ISBN 10: 3031047796
• ISBN 13: 9783031047794
• Binding: Taschenbuch
• Condition: Neu
• Dimensions: 240W x 168H x 11D millimeters 240 millimeters width by 168 millimeters height by 11 millimeters depth
• Weight: 408 grams

About this title

Synopsis

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.

About the Author

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.