Documents disponibles dans la collection

Stability and control of aircraft systems / Langton, Roy

Public ISBD Titre : Stability and control of aircraft systems : introduction to classical feedback control Type de document : texte imprimé Auteurs : Langton, Roy, Auteur Editeur : New York : Wiley Année de publication : 2006 Collection : Aerospace series Importance : 238 p. Présentation : ill. Format : 24 cm ISBN/ISSN/EAN : 978-0-470-01891-0 Note générale : Index Langues : Français (fre) Mots-clés : Stability  of  airplanes Airplanes  --  Control Avions  --  Stabilité Avions  --  Systèmes  de  commande Index. décimale : 629.7 Ingénierie du transport aérien et spatial.Aéronautique et aéronefs.Fusées et missiles.Astronautique et engins spatiaux Résumé : In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of today's products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood. Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples.* Clarifies the design and development of feedback control systems * Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background * Illustrated throughout with figures and tables Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance Stability and control of aircraft systems : introduction to classical feedback control [texte imprimé] / Langton, Roy, Auteur . - Wiley, 2006 . - 238 p. : ill. ; 24 cm. - (Aerospace series) . ISBN : 978-0-470-01891-0 Index Langues : Français (fre) Mots-clés : Stability  of  airplanes Airplanes  --  Control Avions  --  Stabilité Avions  --  Systèmes  de  commande Index. décimale : 629.7 Ingénierie du transport aérien et spatial.Aéronautique et aéronefs.Fusées et missiles.Astronautique et engins spatiaux Résumé : In the current climate of increasing complexity and functional integration in all areas of engineering and technology, stability and control are becoming essential ingredients of engineering knowledge. Many of today's products contain multiple engineering technologies, and what were once simple mechanical, hydraulic or pneumatic products now contain integrated electronics and sensors. Control theory reduces these widely varied technical components into their important dynamic characteristics, expressed as transfer functions, from which the subtleties of dynamic behaviours can be analyzed and understood. Stability and Control of Aircraft Systems is an easy-to-read and understand text that describes control theory using minimal mathematics. It focuses on simple rules, tools and methods for the analysis and testing of feedback control systems using real systems engineering design and development examples.* Clarifies the design and development of feedback control systems * Communicates the theory in an accessible manner that does not require the reader to have a strong mathematical background * Illustrated throughout with figures and tables Stability and Control of Aircraft Systems provides both the seasoned engineer and the graduate with the know-how necessary to minimize problems with fielded systems in the area of operational performance

Exemplaires

Code-barres	Cote	Support	Localisation	Section	Disponibilité	Etat_Exemplaire
053757	629.7 LAN	Papier	Bibliothèque Centrale	Ingénierie	Disponible	Consultation sur place

Advanced control of aircraft, spacecraft, and rockets / Ashish Tewari

Public ISBD Titre : Advanced control of aircraft, spacecraft, and rockets Type de document : texte imprimé Auteurs : Ashish Tewari, Auteur Editeur : New York : Wiley Année de publication : 2011 Collection : Aerospace series Importance : XVII, 436 p. Présentation : ill. Format : 26 cm. ISBN/ISSN/EAN : 978-0-470-74563-2 Note générale : Bibliogr. en fin de chapitres. index Langues : Anglais (eng) Mots-clés : Véhicules  spatiaux  --  Systèmes  de  télécommande Systèmes  de  commande  (vol) Avions  --  Systèmes  de  commande Index. décimale : 629.7 Ingénierie du transport aérien et spatial.Aéronautique et aéronefs.Fusées et missiles.Astronautique et engins spatiaux Résumé : "Advanced Control of Aircraft, Missiles and Spacecraft introduces the reader to the concepts of modern control theory applied to the design and analysis of general flight control systems in a concise and mathematically rigorous style. It presents a comprehensive treatment of both atmospheric and space flight control systems including aircraft, rockets (missiles and launch vehicles), entry vehicles and spacecraft (both orbital and attitude control). The broad coverage of topics emphasizes the synergies among the various flight control systems and attempts to show their evolution from the same set of physical principles as well as their design and analysis by similar mathematical tools. In addition, this book presents state-of-art control system design methods - including multivariable, optimal, robust, digital and nonlinear strategies - as applied to modern flight control systems.Advanced Control of Aircraft, Missiles and Spacecraft features worked-out examples and problems at the end of each chapter as well as a number of MATLAB/ SIMULINK examples that are realistic and representative of the state-of-the-art in flight control"-- "This book presents state-of-art control system design methods - including multivariable, optimal, robust, digital and nonlinear strategies - as applied to modern flight control systems". Note de contenu : Summary : 1. Introduction. 2. Optimal Control Techniques. 3. Optimal Navigation and Control of Aircraft. 4. Optimal Guidance of Rockets. 5. Attitude Control of Rockets. 6. Spacecraft Guidance Systems. 7. Optimal Spacecraft Attitude Control. Advanced control of aircraft, spacecraft, and rockets [texte imprimé] / Ashish Tewari, Auteur . - Wiley, 2011 . - XVII, 436 p. : ill. ; 26 cm.. - (Aerospace series) . ISBN : 978-0-470-74563-2 Bibliogr. en fin de chapitres. index Langues : Anglais (eng) Mots-clés : Véhicules  spatiaux  --  Systèmes  de  télécommande Systèmes  de  commande  (vol) Avions  --  Systèmes  de  commande Index. décimale : 629.7 Ingénierie du transport aérien et spatial.Aéronautique et aéronefs.Fusées et missiles.Astronautique et engins spatiaux Résumé : "Advanced Control of Aircraft, Missiles and Spacecraft introduces the reader to the concepts of modern control theory applied to the design and analysis of general flight control systems in a concise and mathematically rigorous style. It presents a comprehensive treatment of both atmospheric and space flight control systems including aircraft, rockets (missiles and launch vehicles), entry vehicles and spacecraft (both orbital and attitude control). The broad coverage of topics emphasizes the synergies among the various flight control systems and attempts to show their evolution from the same set of physical principles as well as their design and analysis by similar mathematical tools. In addition, this book presents state-of-art control system design methods - including multivariable, optimal, robust, digital and nonlinear strategies - as applied to modern flight control systems.Advanced Control of Aircraft, Missiles and Spacecraft features worked-out examples and problems at the end of each chapter as well as a number of MATLAB/ SIMULINK examples that are realistic and representative of the state-of-the-art in flight control"-- "This book presents state-of-art control system design methods - including multivariable, optimal, robust, digital and nonlinear strategies - as applied to modern flight control systems". Note de contenu : Summary : 1. Introduction. 2. Optimal Control Techniques. 3. Optimal Navigation and Control of Aircraft. 4. Optimal Guidance of Rockets. 5. Attitude Control of Rockets. 6. Spacecraft Guidance Systems. 7. Optimal Spacecraft Attitude Control.

Exemplaires

Code-barres	Cote	Support	Localisation	Section	Disponibilité	Etat_Exemplaire
053338	629.7 TEW	Papier	Bibliothèque Centrale	Génie Mécanique	Disponible	Consultation sur place

Basic helicopter aerodynamics / John Seddon

Public ISBD Titre : Basic helicopter aerodynamics Type de document : texte imprimé Auteurs : John Seddon, Auteur ; Simon Newman, Auteur Mention d'édition : 3 éd Editeur : New York : Wiley Année de publication : 2011 Collection : Aerospace series Importance : 255 p. Présentation : ill. Format : 25 cm ISBN/ISSN/EAN : 978-0-470-66501-5 Note générale : Bibliogr. - Index Langues : Anglais (eng) Mots-clés : Rotors  (hélicoptères)  --  Aérodynamique Rotor  Mechanisms Index. décimale : 629.735.4 Aéronefs à rotors. Hélicoptère Résumé : Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to the first principles of the aerodynamics of helicopter flight. Simon Newman has brought this third edition completely up to date with a full new set of illustrations and imagery. Simon Newman addresses the unique considerations applicable to rotor UAVs and MAVs, and coverage of blade dynamics is expanded to include both flapping, lagging and ground resonance. New material is included on blade tip design, flow characteristics surrounding the rotor in forward flight, tail rotors, brown-out, blade sailing and shipborne operations. Concentrating on the well-known Sikorsky configuration of single main rotor with tail rotor, early chapters deal with the aerodynamics of the rotor in hover, vertical flight, forward flight and climb. Analysis of these motions is developed to the stage of obtaining the principal results for thrust, power and associated quantities. Later chapters turn to the characteristics of the overall helicopter, its performance, stability and control, and the important field of aerodynamic research is discussed, with some reference also to aerodynamic design practice. This introductory level treatment to the aerodynamics of helicopter flight will appeal to aircraft design engineers and undergraduate and graduate students in aircraft design, as well as practising engineers looking for an introduction to or refresher course on the subject. Note de contenu : Au sommaire: 1. Rotor in Vertical Flight: Momentum Theory and Wake Analysis 2. Rotor in Vertical Flight: Blade Element Theory 3. Rotor Mechanisms for Forward Flight. 4. Rotor Aerodynamics in Forward Flight 5. Aerodynamic Design 6. Performance 7. Trim, Stability and Control 8. A Personal Look at the Future Basic helicopter aerodynamics [texte imprimé] / John Seddon, Auteur ; Simon Newman, Auteur  . -  3 éd . - Wiley, 2011 . - 255 p. : ill. ; 25 cm. - (Aerospace series) . ISBN : 978-0-470-66501-5 Bibliogr. - Index Langues : Anglais (eng) Mots-clés : Rotors  (hélicoptères)  --  Aérodynamique Rotor  Mechanisms Index. décimale : 629.735.4 Aéronefs à rotors. Hélicoptère Résumé : Basic Helicopter Aerodynamics is widely appreciated as an easily accessible, rounded introduction to the first principles of the aerodynamics of helicopter flight. Simon Newman has brought this third edition completely up to date with a full new set of illustrations and imagery. Simon Newman addresses the unique considerations applicable to rotor UAVs and MAVs, and coverage of blade dynamics is expanded to include both flapping, lagging and ground resonance. New material is included on blade tip design, flow characteristics surrounding the rotor in forward flight, tail rotors, brown-out, blade sailing and shipborne operations. Concentrating on the well-known Sikorsky configuration of single main rotor with tail rotor, early chapters deal with the aerodynamics of the rotor in hover, vertical flight, forward flight and climb. Analysis of these motions is developed to the stage of obtaining the principal results for thrust, power and associated quantities. Later chapters turn to the characteristics of the overall helicopter, its performance, stability and control, and the important field of aerodynamic research is discussed, with some reference also to aerodynamic design practice. This introductory level treatment to the aerodynamics of helicopter flight will appeal to aircraft design engineers and undergraduate and graduate students in aircraft design, as well as practising engineers looking for an introduction to or refresher course on the subject. Note de contenu : Au sommaire: 1. Rotor in Vertical Flight: Momentum Theory and Wake Analysis 2. Rotor in Vertical Flight: Blade Element Theory 3. Rotor Mechanisms for Forward Flight. 4. Rotor Aerodynamics in Forward Flight 5. Aerodynamic Design 6. Performance 7. Trim, Stability and Control 8. A Personal Look at the Future

Exemplaires

Code-barres	Cote	Support	Localisation	Section	Disponibilité	Etat_Exemplaire
054219	629.735.4 SED	Papier	Bibliothèque Centrale	Génie Mécanique	Disponible	Consultation sur place