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Advances in Aerospace Guidance, Navigation and Control: Selected Papers of the Second CEAS Specialist Conference on Guidance, Navigation and Control

Kataloginformation Katalogdatensatz500178817 .

Kataloginformation
Feldname	Details
Vorliegende Sprache	eng
Hinweise auf parallele Ausgaben	386778264 Druckausg.: ‡Advances in aerospace guidance, navigation and control
ISBN	978-3-642-38252-9
Name	Chu, Qiping
Name	Mulder, Bob
Name ANZEIGE DER KETTE	Mulder, Bob
Name	Choukroun, Daniel
	Kampen, Erik-Jan
	Visser, Coen
	Looye, Gertjan
T I T E L	Advances in Aerospace Guidance, Navigation and Control
Zusatz zum Titel	Selected Papers of the Second CEAS Specialist Conference on Guidance, Navigation and Control
Verlagsort	Berlin ; Heidelberg
Verlag	Springer
Erscheinungsjahr	2013
Erscheinungsjahr	2013
Umfang	Online-Ressource (XX, 782 p. 414 illus, digital)
Reihe	SpringerLink. Bücher
Notiz / Fußnoten	Includes bibliographical references and index
Weiterer Inhalt	Preface; Editorial Committee; Contents; Part I Guidance and Control; Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L2-normFramework; 1 Introduction; 2 Theoretical Background; 2.1 LPV Systems; 2.2 LPV Controller Synthesis; 3 LPV Controller Design for the Missile Model; 3.1 LPV Modeling; 3.2 Controller Design; 3.3 Optimization of the Weighting Functions; 4 Nonlinear Simulations; 5 Discussion and Conclusion; References; Improving the Performance of an Actuator Control Scheme during Saturation; 1 Introduction; 2 Description of Control Scheme. 2.1 Conventional Control Scheme2.2 Proposed Control Scheme; 3 Comparison of Control Schemes; 3.1 Non Saturation Case; 3.2 One Actuator Saturation Case; 4 Simulation; 4.1 Simulation Model; 4.2 Simulation Results; 5 Conclusion; References; Concurrent Learning Adaptive Model Predictive Control; 1 Introduction; 2 Approximate Model Inversion Based Model Reference Adaptive Control; 3 Feedback Linearization for MPC; 3.1 Stability; 4 Model Predictive Control; 5 Trajectory Tracking in the Presence ofWing Rock Dynamics; 6 Conclusion; References. Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part I1 Introduction; 2 Development of the Adaptive Error System Using "Undelayed Ideal Trajectories"; 2.1 Ideal Trajectories; 2.2 Fixed Gain Controller; 2.3 The Adaptive Controller; 3 Robustness of the Adaptive Error System; 4 Simulation and Results; 4.1 Step Disturbances; 5 Conclusions; References; Model Reference Adaptive Control of Mildly Non-Linear Systems with Time Varying Input Delays - Part II; 1 Introduction; 2 Robustness of the Adaptive Error System; 3 Simulation and Results. 3.1 Step Disturbances4 Conclusions; References; Flight Control Algorithms for a Vertical Launch Air Defense Missile; 1 Introduction; 2 Modeling of the Vertical Launch Missile Dynamics; 2.1 Aerodynamic Forces and Moments; 2.2 Thrust Forces and Moments; 3 Autopilot Model; 3.1 Linearized Systems; 3.2 Thrust Vector-Aerodynamic Control Effectiveness; 3.3 Autopilot Simulations; 4 Guidance Algorithms; 4.1 Guidance and Control Simulations; 5 Turnover Strategy; 6 Discussion and Conclusion; References; LFT Model Generation via l1-RegularizedLeast Squares; 1 Introduction; 2 Problem Statement. 3 Polynomial Approximation byRegularized Least Squares; 4 Procedure for the Generation of LFT Models; 4.1 Weighting of the Elements; 4.2 Weighting of the Polynomial Coefficients; 5 Example: Missile Model; 5.1 Generation of the LFR Model; 5.2 Model Assessment; 6 Conclusion; References; An Impulsive Input Approach to Short Time Convergent Control for Linear Systems; 1 Introduction and Motivation; 2 Problem Formulation; 3 The Impulsive Input Approach; 3.1 A; Approximation with Bounded Support; 3.2 A Gaussian Function Approximation; 3.3 A Piecewise-Constant Function Approximation. 4 Comparing the Impulsive Input Approach with the Direct Approach. 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.
Titelhinweis	Druckausg.: ‡Advances in aerospace guidance, navigation and control
ISBN	ISBN 978-3-642-38253-6
Klassifikation	TRP
	TTDS
	TEC002000
	629.1
	TL787-4050.22
	ZO 7630
Kurzbeschreibung	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.
1. Schlagwortkette	Luftfahrzeug
	Raumflugkörper
	Flugführung
	Flugnavigation
	Avionik
	Kongress
ANZEIGE DER KETTE	Luftfahrzeug -- Raumflugkörper -- Flugführung -- Flugnavigation -- Avionik -- Kongress
SWB-Titel-Idn	381840875
Signatur	Springer E-Book
Bemerkungen	Elektronischer Volltext - Campuslizenz
Elektronische Adresse	$uhttp://dx.doi.org/10.1007/978-3-642-38253-6
Internetseite / Link	Volltext
Siehe auch	Inhaltstext
Siehe auch	Volltext
Siehe auch	Cover

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