| Titre : |
Flight stability and automatic control |
| Type de document : |
texte imprimé |
| Auteurs : |
Nelson Robert C., Auteur |
| Editeur : |
New York : McGraw-Hill |
| Année de publication : |
1989 |
| Importance : |
XII-284 p. |
| Présentation : |
ill. |
| Format : |
25 cm |
| ISBN/ISSN/EAN : |
978-0-07-046218-2 |
| Note générale : |
Bibliogr. en fin chapitre |
| Langues : |
Français (fre) |
| Mots-clés : |
Aireplane stabilité--Systeme controle--Automatic control |
| Index. décimale : |
629.7.05 Systemes et instruments de guidage, de controle initial et de navigation |
| Résumé : |
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses. --Ce texte fait référence à l'édition
Many more worked examples and end-of-chapter problems, some of which require computer solutions, are integrated throughout the text.
An expanded section on automatic control theory and its application to flight control system design is now included.
Chapters covering the topics of static stability, flight control, aircraft dynamics, and flying qualities have been improved.
Problems that require the use of a computer are now clearly identified.
Material is introduced by way of simple exercises so students can see how the design process is applied without a lot of mathematical complexity.
Interesting historical notes are presented throughout the text.
The text provides an integrated treatment of aircraft stability, flight control, and autopilot design. --Ce texte fait référence à l'édition |
| Note de contenu : |
Sommaire:
1-Introduction
2-Static Stability and Control
3-Aircraft Equations of Motion
4-Longitudinal Motion (Stick Fixed)
5-Lateral Motion (Stick Fixed)
6-Aircraft Response to Control on Atmospheric Inputs
7-Automatic Control Theory-The Classical Approach
8-Application of Classic Control Theory to Aircraft Autopilot Design
9-Modern Control Theory
10-Applications of Modern Control Theory to Aircraft Autopilot Design |
Flight stability and automatic control [texte imprimé] / Nelson Robert C., Auteur . - New York : McGraw-Hill, 1989 . - XII-284 p. : ill. ; 25 cm. ISBN : 978-0-07-046218-2 Bibliogr. en fin chapitre Langues : Français ( fre)
| Mots-clés : |
Aireplane stabilité--Systeme controle--Automatic control |
| Index. décimale : |
629.7.05 Systemes et instruments de guidage, de controle initial et de navigation |
| Résumé : |
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses. --Ce texte fait référence à l'édition
Many more worked examples and end-of-chapter problems, some of which require computer solutions, are integrated throughout the text.
An expanded section on automatic control theory and its application to flight control system design is now included.
Chapters covering the topics of static stability, flight control, aircraft dynamics, and flying qualities have been improved.
Problems that require the use of a computer are now clearly identified.
Material is introduced by way of simple exercises so students can see how the design process is applied without a lot of mathematical complexity.
Interesting historical notes are presented throughout the text.
The text provides an integrated treatment of aircraft stability, flight control, and autopilot design. --Ce texte fait référence à l'édition |
| Note de contenu : |
Sommaire:
1-Introduction
2-Static Stability and Control
3-Aircraft Equations of Motion
4-Longitudinal Motion (Stick Fixed)
5-Lateral Motion (Stick Fixed)
6-Aircraft Response to Control on Atmospheric Inputs
7-Automatic Control Theory-The Classical Approach
8-Application of Classic Control Theory to Aircraft Autopilot Design
9-Modern Control Theory
10-Applications of Modern Control Theory to Aircraft Autopilot Design |
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