Satellite Formation Flying (Record no. 76474)

000 -LEADER
fixed length control field 03684nam a22005895i 4500
001 - CONTROL NUMBER
control field 978-981-15-9631-5
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801214542.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 210315s2021 si | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9789811596315
-- 978-981-15-9631-5
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Mathavaraj, S.
245 10 - TITLE STATEMENT
Title Satellite Formation Flying
Sub Title High Precision Guidance using Optimal and Adaptive Control Techniques /
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2021.
300 ## - PHYSICAL DESCRIPTION
Number of Pages XXI, 154 p. 96 illus., 88 illus. in color.
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Chapter 1: Introduction and Motivation -- Chapter 2: Satellite Orbital Dynamics -- Chapter 3: Infinite-time LQR and SDRE for Satellite Formation Flying -- Chapter4: Adaptive LQR for Satellite Formation Flying -- Chapter 5: Adaptive Dynamic Inversion for Satellite Formation Flying -- Chapter 6: Finite-time LQR and SDRE for Satellite Formation Flying -- Chapter 7: Model Predictive Static Programming -- Chapter 8: Performance Comparison.
520 ## - SUMMARY, ETC.
Summary, etc Small satellite technology is opening up a new era in space exploration offering reduced cost of launch and maintenance, operational flexibility with on-orbit reconfiguration, redundancy etc. The true power of such missions can be harnessed only from close and precise formation flying of satellites. Formation flying missions support diverse application areas such as reconnaissance, remote sensing, solar observatory, deep space observatories, etc. A key component involved in formation flying is the guidance algorithm that should account for system nonlinearities and unknown disturbances. The main focus of this book is to present various nonlinear optimal control and adaptive guidance ideas to ensure precise close formation flying in presence of such difficulties. In addition to in-depth discussion of the relevant topics, MATLAB program files for the results included are also provided for the benefit of the readers. Since this book has concise information about the various guidance techniques, it will be useful reference for researchers and practising engineers in the space field.
700 1# - AUTHOR 2
Author 2 Padhi, Radhakant.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-981-15-9631-5
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Singapore :
-- Springer Nature Singapore :
-- Imprint: Springer,
-- 2021.
336 ## -
-- text
-- txt
-- rdacontent
337 ## -
-- computer
-- c
-- rdamedia
338 ## -
-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Multibody systems.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Vibration.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mechanics, Applied.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mathematical optimization.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Multibody Systems and Mechanical Vibrations.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Optimization.
912 ## -
-- ZDB-2-ENG
912 ## -
-- ZDB-2-SXE

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