Compound Control Methodology for Flight Vehicles (Record no. 55475)

000 -LEADER
fixed length control field 03126nam a22004935i 4500
001 - CONTROL NUMBER
control field 978-3-642-36841-7
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20200421111839.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 130607s2013 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783642368417
-- 978-3-642-36841-7
082 04 - CLASSIFICATION NUMBER
Call Number 629.8
100 1# - AUTHOR NAME
Author Xia, Yuanqing.
245 10 - TITLE STATEMENT
Title Compound Control Methodology for Flight Vehicles
300 ## - PHYSICAL DESCRIPTION
Number of Pages XVIII, 260 p. 125 illus.
490 1# - SERIES STATEMENT
Series statement Lecture Notes in Control and Information Sciences,
505 0# - FORMATTED CONTENTS NOTE
Remark 2 Overview of Sliding Mode Control -- Overview of Active Disturbance Rejection Control -- Overview of Flight Vehicle Control -- The Descriptions of Flight Vehicle -- SMC for Missile Systems Based on Back-Stepping and ESO Techniques -- Adaptive SMC for Attitude Stabilization in Presence of Actuator Saturation -- Adaptive Nonsingular Terminal Sliding Mode Control for Rigid Spacecraft -- Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances -- SMC for Attitude Tracking of Rigid Spacecraft with Disturbances -- Missile Guidance Law Based on ESO Techniques -- Missile Guidance Laws Based on SMC and FTC Techniques -- Cooperative Attack of Multiple Missiles Based on Optimal Guidance Law.
520 ## - SUMMARY, ETC.
Summary, etc "Compound Control Methodology for Flight Vehicles" focuses on new control methods for flight vehicles. In this monograph the concept of compound control is introduced. It is demonstrated that both Sliding Mode Control (SMC) and Active Disturbance Rejection Control (ADRC) have their own advantages and limitations, i.e., chattering of SMC and the observability of extended state observer (ESO), respectively. It is shown that compound control combines their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle control.
700 1# - AUTHOR 2
Author 2 Fu, Mengyin.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-642-36841-7
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Berlin, Heidelberg :
-- Springer Berlin Heidelberg :
-- Imprint: Springer,
-- 2013.
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-- text
-- txt
-- rdacontent
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-- computer
-- c
-- rdamedia
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-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Control engineering.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Engineering.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Control.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE
-- 0170-8643 ;
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-- ZDB-2-ENG

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