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Advances in Aerospace Guidance, Navigation and Control (Record no. 12292)

000 -LEADER
fixed length control field 04324nam a22004455i 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20140310143356.0
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 130427s2013 gw | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number 9783642382536
978-3-642-38253-6
082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 629.1
Edition number 23
264 #1 -
-- Berlin, Heidelberg :
-- Springer Berlin Heidelberg :
-- Imprint: Springer,
-- 2013.
912 ## -
-- ZDB-2-ENG
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Chu, Qiping.
Relator term editor.
245 10 - IMMEDIATE SOURCE OF ACQUISITION NOTE
Title Advances in Aerospace Guidance, Navigation and Control
Medium [electronic resource] :
Remainder of title Selected Papers of the Second CEAS Specialist Conference on Guidance, Navigation and Control /
Statement of responsibility, etc edited by Qiping Chu, Bob Mulder, Daniel Choukroun, Erik-Jan Kampen, Coen Visser, Gertjan Looye.
300 ## - PHYSICAL DESCRIPTION
Extent XX, 782 p. 414 illus.
Other physical details online resource.
505 0# - FORMATTED CONTENTS NOTE
Formatted contents note Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L2-norm Framework -- L2-norm Framework -- Improving the performance of an actuator control scheme during saturation -- Concurrent Learning Adaptive Model Predictive Control -- Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part I Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part II LFT model generation via `1-regularized least squares -- An Impulsive Input Approach to Short Time Convergent Control for Linear Systems -- Model Formulation of Pursuit Problem with Two Pursuers and One Evader -- Nonlinear Output-Feedback H¥ Control for Spacecraft Attitude Control.
520 ## - SUMMARY, ETC.
Summary, etc Following the successful 1st CEAS (Council of European Aerospace Societies) Specialist Conference on Guidance, Navigation and Control (CEAS EuroGNC) held in Munich, Germany in 2011, Delft University of Technology happily accepted the invitation of organizing the 2nd  CEAS EuroGNC in Delft, The Netherlands in 2013. The goal of the conference is to promote new advances in aerospace GNC theory and technologies for enhancing safety, survivability, efficiency, performance, autonomy and intelligence of aerospace systems using on-board sensing, computing and systems. A great push for new developments in GNC are the ever higher safety and sustainability requirements in aviation. Impressive progress was made in new research fields such as sensor and actuator fault detection and diagnosis, reconfigurable and fault tolerant flight control, online safe flight envelop prediction and protection, online global aerodynamic model identification, online global optimization and flight upset recovery. All of these challenges depend on new online solutions from on-board computing systems. Scientists and engineers in GNC have been developing model based, sensor based as well as knowledge based approaches aiming for highly robust, adaptive, nonlinear, intelligent and autonomous GNC systems. Although the papers presented at the conference and selected in this book could not possibly cover all of the present challenges in the GNC field, many of them have indeed been addressed and a wealth of new ideas, solutions and results were proposed and presented. For the 2nd CEAS Specialist Conference on Guidance, Navigation and Control the International Program Committee conducted a formal review process. Each paper was reviewed in compliance with good journal practice by at least two independent and anonymous reviewers. The papers published in this book were selected from the conference proceedings based on the results and recommendations from the reviewers.    
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name as entry element Engineering.
Topical term or geographic name as entry element Astronautics.
Topical term or geographic name as entry element Engineering.
Topical term or geographic name as entry element Aerospace Technology and Astronautics.
Topical term or geographic name as entry element Control.
700 1# - ADDED ENTRY--PERSONAL NAME
Personal name Mulder, Bob.
Relator term editor.
Personal name Choukroun, Daniel.
Relator term editor.
Personal name Kampen, Erik-Jan.
Relator term editor.
Personal name Visser, Coen.
Relator term editor.
Personal name Looye, Gertjan.
Relator term editor.
710 2# - ADDED ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element SpringerLink (Online service)
773 0# - HOST ITEM ENTRY
Title Springer eBooks
776 08 - ADDITIONAL PHYSICAL FORM ENTRY
Display text Printed edition:
International Standard Book Number 9783642382529
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier http://dx.doi.org/10.1007/978-3-642-38253-6
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Item type E-Book
Copies
Price effective from Permanent location Date last seen Not for loan Date acquired Source of classification or shelving scheme Koha item type Damaged status Lost status Withdrawn status Current location Full call number
2014-04-03AUM Main Library2014-04-03 2014-04-03 E-Book   AUM Main Library629.1

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