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Flight dynamics principles /
The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Amsterdam ; Boston :
Elsevier/Butterworth-Heinemann,
2007.
|
| Edición: | 2nd ed. |
| Colección: | Elsevier aerospace engineering series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 049 | |a UAMI | ||
| 100 | 1 | |a Cook, M. V. | |
| 245 | 1 | 0 | |a Flight dynamics principles / |c M.V. Cook. |
| 250 | |a 2nd ed. | ||
| 260 | |a Amsterdam ; |a Boston : |b Elsevier/Butterworth-Heinemann, |c 2007. | ||
| 300 | |a 1 online resource (xxi, 468 pages) : |b illustrations | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Elsevier aerospace engineering series | |
| 504 | |a Includes bibliographical references and index. | ||
| 588 | 0 | |a Print version record. | |
| 505 | 0 | 0 | |t Flight Dynamics Principles -- |t Copyright page -- |t Preface to the first edition -- |t Preface to the second edition -- |t Nomenclature -- |g 1. |t Introduction -- |g 1.1. |t Overview -- |g 1.2. |t Flying and handling qualities -- |g 1.3. |t General considerations -- |g 1.4. |t Aircraft equations of motion -- |g 1.5. |t Aerodynamics -- |g 1.6. |t Computers -- |g 1.7. |t Summary -- |g 2. |t Systems of axes and notation -- |g 2.1. |t Earth axes -- |g 2.2. |t Aircraft body fixed axes -- |g 2.3. |t Euler angles and aircraft attitude -- |g 2.4. |t Axes transformations -- |g 2.5. |t Aircraft reference geometry -- |g 2.6. |t Controls notation -- |g 2.7. |t Aerodynamic reference centres |
| 505 | 0 | 0 | |g 5.1. |t Methods of solution -- |g 5.2. |t Cramer's rule -- |g 5.3. |t Aircraft response transfer functions -- |g 5.4. |t Response to controls -- |g 5.5. |t Acceleration response transfer functions -- |g 5.6. |t The state space method -- |g 5.7. |t State space model augmentation -- |t Problems -- |g 6. |t Longitudinal dynamics -- |g 6.1. |t Response to controls -- |g 6.2. |t The dynamic stability modes -- |g 6.3. |t Reduced order models -- |g 6.4. |t Frequency response -- |g 6.5. |t Flying and handling qualities -- |g 6.6. |t Mode excitation -- |t Problems -- |g 7. |t Lateral-directional dynamics -- |g 7.1. |t Response to controls -- |g 7.2. |t The dynamic stability modes -- |g 7.3. |t Reduced order models |
| 505 | 0 | 0 | |g 7.4. |t Frequency response -- |g 7.5. |t Flying and handling qualities -- |g 7.6. |t Mode excitation -- |t Problems -- |g 8. |t Manoeuvrability -- |g 8.1. |t Introduction -- |g 8.2. |t The steady pull-up manoeuvre -- |g 8.3. |t The pitching moment equation -- |g 8.4. |t Longitudinal manoeuvre stability -- |g 8.5. |t Aircraft dynamics and manoeuvrability -- |g 9. |t Stability -- |g 9.1. |t Introduction -- |g 9.2. |t The characteristic equation -- |g 9.3. |t The Routh-Hurwitz stability criterion -- |g 9.4. |t The stability quartic -- |g 9.5. |t Graphical interpretation of stability -- |t Problems -- |g 10. |t Flying and handling qualities -- |g 10.1. |t Introduction |
| 505 | 0 | 0 | |g 10.2. |t Short term dynamic models -- |g 10.3. |t Flying qualities requirements -- |g 10.4. |t Aircraft role -- |g 10.5. |t Pilot opinion rating -- |g 10.6. |t Longitudinal flying qualities requirements -- |g 10.7. |t Control anticipation parameter -- |g 10.8. |t Lateral-directional flying qualities requirements -- |g 10.9. |t Flying qualities requirements on the s-plane -- |t Problems -- |g 11. |t Stability augmentation -- |g 11.1. |t Introduction -- |g 11.2. |t Augmentation system design -- |g 11.3. |t Closed loop system analysis -- |g 11.4. |t The root locus plot -- |g 11.5. |t Longitudinal stability augmentation -- |g 11.6. |t Lateral-directional stability augmentation -- |g 11.7. |t The pole placement method. |
| 520 | |a The study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for tho. | ||
| 590 | |a eBooks on EBSCOhost |b EBSCO eBook Subscription Academic Collection - Worldwide | ||
| 650 | 0 | |a Aerodynamics. | |
| 650 | 0 | |a Flight control. | |
| 650 | 0 | |a Stability of airplanes. | |
| 650 | 6 | |a Aérodynamique. | |
| 650 | 6 | |a Systèmes de commande (Vol) | |
| 650 | 6 | |a Avions |x Stabilité. | |
| 650 | 7 | |a aerodynamics. |2 aat | |
| 650 | 7 | |a TRANSPORTATION |x Aviation |x General. |2 bisacsh | |
| 650 | 7 | |a Aerodynamics |2 fast | |
| 650 | 7 | |a Flight control |2 fast | |
| 650 | 7 | |a Stability of airplanes |2 fast | |
| 776 | 0 | 8 | |i Print version: |a Cook, M.V. |t Flight dynamics principles. |b 2nd ed. |d Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, 2007 |z 0750669276 |z 9780750669276 |w (OCoLC)171268192 |
| 830 | 0 | |a Elsevier aerospace engineering series. | |
| 856 | 4 | 0 | |u https://ebsco.uam.elogim.com/login.aspx?direct=true&scope=site&db=nlebk&AN=203095 |z Texto completo |
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| 994 | |a 92 |b IZTAP | ||