Principles of Spacecraft Control (Registro nro. 260450)

MARC details
000 -LIDER
fixed length control field 04148nam a22005295i 4500
001 - CONTROL NUMBER
control field 978-3-031-04780-0
003 - CONTROL NUMBER IDENTIFIER
control field DE-He213
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20240207153450.0
007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION
fixed length control field cr nn 008mamaa
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 221011s2023 sz | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9783031047800
-- 978-3-031-04780-0
050 #4 - LIBRARY OF CONGRESS CALL NUMBER
Classification number TL1-4050
072 #7 - SUBJECT CATEGORY CODE
Subject category code TR
Source bicssc
072 #7 - SUBJECT CATEGORY CODE
Subject category code TEC009070
Source bisacsh
072 #7 - SUBJECT CATEGORY CODE
Subject category code TR
Source thema
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 620
Edition number 23
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Fichter, Walter.
Relator term author.
Relator code aut
-- http://id.loc.gov/vocabulary/relators/aut
245 10 - TITLE STATEMENT
Title Principles of Spacecraft Control
Medium [electronic resource] :
Remainder of title Concepts and Theory for Practical Applications /
Statement of responsibility, etc. by Walter Fichter, Ramin T. Geshnizjani.
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2023.
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2023.
300 ## - PHYSICAL DESCRIPTION
Extent XVII, 193 p. 63 illus., 24 illus. in color.
Other physical details online resource.
336 ## -
-- text
-- txt
-- rdacontent
337 ## -
-- computer
-- c
-- rdamedia
338 ## -
-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
500 ## - GENERAL NOTE
General note Acceso multiusuario
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note System Engineering Basics -- Satellite Motion Models -- Rotational State Determination -- Actuator Commanding -- Attitude and Momentum Control -- Accelerometers and Drag-Free Control -- Closing Remarks.
520 ## - SUMMARY, ETC.
Summary, etc. 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.
541 ## - IMMEDIATE SOURCE OF ACQUISITION NOTE
Owner UABC ;
Method of acquisition Perpetuidad
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Término temático o nombre geográfico como elemento de entrada Vehicles.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Término temático o nombre geográfico como elemento de entrada Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Término temático o nombre geográfico como elemento de entrada Astronautics.
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Término temático o nombre geográfico como elemento de entrada Vehicle Engineering.
650 24 - SUBJECT ADDED ENTRY--TOPICAL TERM
Término temático o nombre geográfico como elemento de entrada Aerospace Technology and Astronautics.
700 1# - ADDED ENTRY--PERSONAL NAME
Personal name Geshnizjani, Ramin T.
Relator term author.
Relator code aut
-- http://id.loc.gov/vocabulary/relators/aut
710 2# - ADDED ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element SpringerLink (Online service)
773 0# - HOST ITEM ENTRY
Title Springer Nature eBook
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Relationship information Printed edition:
International Standard Book Number 9783031047794
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Relationship information Printed edition:
International Standard Book Number 9783031047817
856 40 - ELECTRONIC LOCATION AND ACCESS
Public note Libro electrónico
Uniform Resource Identifier http://libcon.rec.uabc.mx:2048/login?url=https://doi.org/10.1007/978-3-031-04780-0
912 ## -
-- ZDB-2-ENG
912 ## -
-- ZDB-2-SXE
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Libro Electrónico
Existencias
Estado de retiro Colección Ubicación permanente Ubicación actual Fecha de ingreso Total Checkouts Date last seen Número de copia Tipo de material
  Colección de Libros Electrónicos Biblioteca Electrónica Biblioteca Electrónica 07/02/2024   07/02/2024 1 Libro Electrónico

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