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Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham
| Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham |
| Autore | Grunn Emmanuel |
| Pubbl/distr/stampa | London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 |
| Descrizione fisica | 1 online resource (124 p.) |
| Disciplina | 629.13230151 |
| Altri autori (Persone) | PhạmAnh Tuan (Engineer) |
| Collana | Automation-control and industrial engineering series |
| Soggetto topico |
Aerodynamics - Mathematics
System analysis - Mathematical models |
| ISBN |
1-118-57986-0
1-118-57997-6 1-118-58007-9 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title Page; Table of Contents; Introduction; Chapter 1. 0D Analytical Modeling of Airplane Motions; 1.1. References: axis systems on use; 1.1.1. Galilean reference: R0; 1.1.2. Airplane reference: RB (body) also called "linked reference"; 1.1.3. Resultant angular velocity; 1.2. Equations of motion of the airplane; 1.2.1. Expression of Newton's principle; 1.2.2. Expression of the dynamic momentum; 1.3. Description of external forces and torques; 1.3.1. Aerodynamic forces and torques; 1.3.2. Sign rules; 1.4. Description of aerodynamic coefficients; 1.4.1. Drag coefficient: Cx
1.4.2. Side lift coefficient: CY1.4.3. Vertical lift due to attack angle: CZα; 1.4.4. Lift due to pitch angular velocity: CZq; 1.4.5. Roll coefficients (due to β, δl , p); 1.4.6. Pitch coefficients (due to α, δm , q , static curvature); 1.4.7. Yaw coefficients (due to β, δn, r); 1.5. Aerodynamic data of a supersonic airliner for valuation of the software; 1.6. Horizontal flight as an initial condition; 1.7. Effect of gravitational forces; 1.8 calculation of the trajectory of the airplane in open space; 1.9. Validation by comparison with ONERA Concorde data 1.10. Definitions of aerodynamic coefficients and derivatives 1.10.1.1.10.1. Aerodynamic coefficients; 1.10.2. Total lift coefficient; 1.10.3. Drag characteristics: (dimensionless); 1.10.4. Side lift coefficient: CY (dimensionless); 1.10.5. Roll coefficients; 1.10.6. Pitch coefficients; 1.10.7. Yaw coefficients; Chapter 2. Design and Optimization of anUnmanned Aerial Vehicle (UAV); 2.1. General design of the drone; 2.2. Weight estimation; 2.3. Size estimation; 2.4. Mass and inertia evaluation; 2.4.1. Mass evaluation; 2.4.2. Measurement of the roll inertia (A) 2.4.3. Measurement of pitch inertia (B)2.4.4. Measurement of yaw inertia (C); 2.5. Convergence toward the target; Chapter 3. Organization of the Auto-Pilot; 3.1. Position of the drone in open space; 3.2. The Dog Law; 3.3. Flight tests; 3.4. Altitude control system; 3.5. Altitude measurement on an actual drone; Bibliography; Index |
| Record Nr. | UNINA-9910140187003321 |
Grunn Emmanuel
|
||
| London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham
| Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham |
| Autore | Grunn Emmanuel |
| Pubbl/distr/stampa | London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 |
| Descrizione fisica | 1 online resource (124 p.) |
| Disciplina | 629.13230151 |
| Altri autori (Persone) | PhạmAnh Tuan (Engineer) |
| Collana | Automation-control and industrial engineering series |
| Soggetto topico |
Aerodynamics - Mathematics
System analysis - Mathematical models |
| ISBN |
1-118-57986-0
1-118-57997-6 1-118-58007-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Cover; Title Page; Table of Contents; Introduction; Chapter 1. 0D Analytical Modeling of Airplane Motions; 1.1. References: axis systems on use; 1.1.1. Galilean reference: R0; 1.1.2. Airplane reference: RB (body) also called "linked reference"; 1.1.3. Resultant angular velocity; 1.2. Equations of motion of the airplane; 1.2.1. Expression of Newton's principle; 1.2.2. Expression of the dynamic momentum; 1.3. Description of external forces and torques; 1.3.1. Aerodynamic forces and torques; 1.3.2. Sign rules; 1.4. Description of aerodynamic coefficients; 1.4.1. Drag coefficient: Cx
1.4.2. Side lift coefficient: CY1.4.3. Vertical lift due to attack angle: CZα; 1.4.4. Lift due to pitch angular velocity: CZq; 1.4.5. Roll coefficients (due to β, δl , p); 1.4.6. Pitch coefficients (due to α, δm , q , static curvature); 1.4.7. Yaw coefficients (due to β, δn, r); 1.5. Aerodynamic data of a supersonic airliner for valuation of the software; 1.6. Horizontal flight as an initial condition; 1.7. Effect of gravitational forces; 1.8 calculation of the trajectory of the airplane in open space; 1.9. Validation by comparison with ONERA Concorde data 1.10. Definitions of aerodynamic coefficients and derivatives 1.10.1.1.10.1. Aerodynamic coefficients; 1.10.2. Total lift coefficient; 1.10.3. Drag characteristics: (dimensionless); 1.10.4. Side lift coefficient: CY (dimensionless); 1.10.5. Roll coefficients; 1.10.6. Pitch coefficients; 1.10.7. Yaw coefficients; Chapter 2. Design and Optimization of anUnmanned Aerial Vehicle (UAV); 2.1. General design of the drone; 2.2. Weight estimation; 2.3. Size estimation; 2.4. Mass and inertia evaluation; 2.4.1. Mass evaluation; 2.4.2. Measurement of the roll inertia (A) 2.4.3. Measurement of pitch inertia (B)2.4.4. Measurement of yaw inertia (C); 2.5. Convergence toward the target; Chapter 3. Organization of the Auto-Pilot; 3.1. Position of the drone in open space; 3.2. The Dog Law; 3.3. Flight tests; 3.4. Altitude control system; 3.5. Altitude measurement on an actual drone; Bibliography; Index |
| Record Nr. | UNINA-9910820286703321 |
|
Grunn Emmanuel
|
||
| London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||