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Modeling of complex systems : application to aeronautical dynamics /
In the field of aeronautical dynamics, this book offers readers a design tool which enables them to solve the different problems that can occur during the planning stage of a private project. The authors present a system for the modeling, design and calculation of the flying qualities of airplanes a...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Otros Autores: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Hoboken :
Wiley,
2013.
|
| Colección: | Focus nanoscience and nanotechnology series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
MARC
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| 100 | 1 | |a Grunn, Emmanuel. | |
| 245 | 1 | 0 | |a Modeling of complex systems : |b application to aeronautical dynamics / |c Emmanuel Grunn, Anh Tuan Pham. |
| 260 | |a Hoboken : |b Wiley, |c 2013. | ||
| 300 | |a 1 online resource (124 pages) | ||
| 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 FOCUS Series | |
| 588 | 0 | |a Print version record. | |
| 504 | |a Includes bibliographical references and index. | ||
| 520 | |a In the field of aeronautical dynamics, this book offers readers a design tool which enables them to solve the different problems that can occur during the planning stage of a private project. The authors present a system for the modeling, design and calculation of the flying qualities of airplanes and drones, with a complete mathematical model by Matlab/Simulink. As such, this book may be useful for design engineers as well as for keen airplane amateurs. The authors expound the various phases involved in the design process of an airplane, starting with the formulation of a design tool. | ||
| 505 | 0 | 0 | |g Machine generated contents note: |g ch. 1 |t 0D Analytical Modeling of the Airplane Motions -- |g 1.1. |t References: axis systems on use -- |g 1.1.1. |t Galilean reference: Ro -- |g 1.1.2. |t Airplane reference: RB (body) also called "linked reference" -- |g 1.1.3. |t Resultant angular velocity -- |g 1.2. |t Equations of motion of the airplane -- |g 1.2.1. |t Expression of Newton's principle -- |g 1.2.2. |t Expression of the dynamic momentum -- |g 1.3. |t Description of external forces and torques -- |g 1.3.1. |t Aerodynamic forces and torques -- |g 1.3.2. |t Sign rules -- |g 1.4. |t Description of aerodynamic coefficients -- |g 1.4.1. |t Drag coefficient: Cx -- |g 1.4.2. |t Side lift coefficient CY -- |g 1.4.3. |t Vertical lift due to attack angle: CZ? -- |g 1.4.4. |t Lift due to pitch angular velocity: CZq -- |g 1.4.5. |t Roll coefficients (due to?,?l, p) -- |g 1.4.6. |t Pitch coefficients (due to?,?m, q, static curvature) -- |g 1.4.7. |t Yaw coefficients (due to?,?n, r) -- |g 1.5. |t Aerodynamic data of a supersonic airliner for valuation of the software -- |g 1.6. |t Horizontal flight as an initial condition -- |g 1.7. |t Effect of gravitational forces -- |g 1.8. |t Calculation of the trajectory of the airplane in open space -- |g 1.9. |t Validation by comparison with ONERA Concorde data -- |g 1.10. |t Definitions of aerodynamic coefficients and derivatives -- |g 1.10.1. |t Aerodynamic coefficients -- |g 1.10.2. |t Total lift coefficient -- |g 1.10.3. |t Drag characteristics: (dimensionless) -- |g 1.10.4. |t Side lift coefficient: CY (dimensionless) -- |g 1.10.5. |t Roll coefficients -- |g 1.10.6. |t Pitch coefficients -- |g 1.10.7. |t Yaw coefficients -- |g ch. 2 |t Design and Optimization of an Unmanned Aerial Vehicle (UAV) -- |g 2.1. |t General design of the drone -- |g 2.2. |t Weight estimation -- |g 2.3. |t Size estimation -- |g 2.4. |t Mass and inertia evaluation -- |g 2.4.1. |t Mass evaluation -- |g 2.4.2. |t Measurement of the roll inertia (A) -- |g 2.4.3. |t Measurement of pitch inertia (B) -- |g 2.4.4. |t Measurement of yaw inertia (C) -- |g 2.5. |t Convergence toward the target -- |g ch. 3 |t Organization of the Auto-Pilot -- |g 3.1. |t Position of the drone in open space -- |g 3.2. |t Dog Law -- |g 3.3. |t Flight tests -- |g 3.4. |t Altitude control system -- |g 3.5. |t Altitude measurement on an actual drone. |
| 590 | |a ProQuest Ebook Central |b Ebook Central Academic Complete | ||
| 650 | 0 | |a Aerodynamics |x Mathematics. | |
| 650 | 0 | |a System analysis |x Mathematical models. | |
| 650 | 6 | |a Aérodynamique |x Mathématiques. | |
| 650 | 6 | |a Analyse de systèmes |x Modèles mathématiques. | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Engineering (General) |2 bisacsh | |
| 650 | 7 | |a Aerodynamics |x Mathematics |2 fast | |
| 650 | 7 | |a System analysis |x Mathematical models |2 fast | |
| 700 | 1 | |a Pham, Anh Tuan |c (Engineer) |1 https://id.oclc.org/worldcat/entity/E39PCjrpfttJfYDjRkwxvrrbcX | |
| 758 | |i has work: |a Modeling of Complex Systems (Text) |1 https://id.oclc.org/worldcat/entity/E39PCFtfB9JVYfyJ6rXqQQ73jP |4 https://id.oclc.org/worldcat/ontology/hasWork | ||
| 776 | 0 | 8 | |i Print version: |a Grunn, Emanuel. |t Modeling of Complex Systems : Application to Aeronautical Dynamics. |d Hoboken : Wiley, ©2013 |z 9781848214484 |
| 830 | 0 | |a Focus nanoscience and nanotechnology series. | |
| 856 | 4 | 0 | |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=1575624 |z Texto completo |
| 880 | 0 | 0 | |6 505-00/(S |g Machine generated contents note: |g ch. 1 |t 0D Analytical Modeling of the Airplane Motions -- |g 1.1. |t References: axis systems on use -- |g 1.1.1. |t Galilean reference: Ro -- |g 1.1.2. |t Airplane reference: RB (body) also called "linked reference" -- |g 1.1.3. |t Resultant angular velocity -- |g 1.2. |t Equations of motion of the airplane -- |g 1.2.1. |t Expression of Newton's principle -- |g 1.2.2. |t Expression of the dynamic momentum -- |g 1.3. |t Description of external forces and torques -- |g 1.3.1. |t Aerodynamic forces and torques -- |g 1.3.2. |t Sign rules -- |g 1.4. |t Description of aerodynamic coefficients -- |g 1.4.1. |t Drag coefficient: Cx -- |g 1.4.2. |t Side lift coefficient CY -- |g 1.4.3. |t Vertical lift due to attack angle: CZα -- |g 1.4.4. |t Lift due to pitch angular velocity: CZq -- |g 1.4.5. |t Roll coefficients (due to β, δl, p) -- |g 1.4.6. |t Pitch coefficients (due to α, δm, q, static curvature) -- |g 1.4.7. |t Yaw coefficients (due to β, δn, r) -- |g 1.5. |t Aerodynamic data of a supersonic airliner for valuation of the software -- |g 1.6. |t Horizontal flight as an initial condition -- |g 1.7. |t Effect of gravitational forces -- |g 1.8. |t Calculation of the trajectory of the airplane in open space -- |g 1.9. |t Validation by comparison with ONERA Concorde data -- |g 1.10. |t Definitions of aerodynamic coefficients and derivatives -- |g 1.10.1. |t Aerodynamic coefficients -- |g 1.10.2. |t Total lift coefficient -- |g 1.10.3. |t Drag characteristics: (dimensionless) -- |g 1.10.4. |t Side lift coefficient: CY (dimensionless) -- |g 1.10.5. |t Roll coefficients -- |g 1.10.6. |t Pitch coefficients -- |g 1.10.7. |t Yaw coefficients -- |g ch. 2 |t Design and Optimization of an Unmanned Aerial Vehicle (UAV) -- |g 2.1. |t General design of the drone -- |g 2.2. |t Weight estimation -- |g 2.3. |t Size estimation -- |g 2.4. |t Mass and inertia evaluation -- |g 2.4.1. |t Mass evaluation -- |g 2.4.2. |t Measurement of the roll inertia (A) -- |g 2.4.3. |t Measurement of pitch inertia (B) -- |g 2.4.4. |t Measurement of yaw inertia (C) -- |g 2.5. |t Convergence toward the target -- |g ch. 3 |t Organization of the Auto-Pilot -- |g 3.1. |t Position of the drone in open space -- |g 3.2. |t Dog Law -- |g 3.3. |t Flight tests -- |g 3.4. |t Altitude control system -- |g 3.5. |t Altitude measurement on an actual drone. |
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