| Titre : |
Advanced control of aircraft, spacecraft, and rockets |
| Type de document : |
texte imprimé |
| Auteurs : |
Ashish Tewari, Auteur |
| Editeur : |
New York : John Wiley & Sons |
| 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
Airplanes--Control systems
Flight control
Rockets (Aeronautics)--Control systems
Space vehicles--Control systems |
| 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 . - New York : John Wiley & Sons, 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
Airplanes--Control systems
Flight control
Rockets (Aeronautics)--Control systems
Space vehicles--Control systems |
| 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. |
|  |
629 Ingénierie des véhicules de transport 
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