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...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Grunn, Emmanuel
Otros Autores: Pham, Anh Tuan (Engineer)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Hoboken : Wiley, 2013.
Colección:Focus nanoscience and nanotechnology series.
Temas:
Aerodynamics > Mathematics.
System analysis > Mathematical models.
Aérodynamique > Mathématiques.
Analyse de systèmes > Modèles mathématiques.
TECHNOLOGY & ENGINEERING > Engineering (General)
Aerodynamics > Mathematics
System analysis > Mathematical models
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Machine generated contents note: ch. 1 0D Analytical Modeling of the Airplane Motions
  • 1.1. References: axis systems on use
  • 1.1.1. Galilean reference: Ro
  • 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 CY
  • 1.4.3. Vertical lift due to attack angle: CZ?
  • 1.4.4. Lift due to pitch angular velocity: CZq
  • 1.4.5. Roll coefficients (due to?,?l, p)
  • 1.4.6. Pitch coefficients (due to?,?m, q, static curvature)
  • 1.4.7. Yaw coefficients (due to?,?n, 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. 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
  • ch. 2 Design and Optimization of an Unmanned 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
  • ch. 3 Organization of the Auto-Pilot
  • 3.1. Position of the drone in open space
  • 3.2. Dog Law
  • 3.3. Flight tests
  • 3.4. Altitude control system
  • 3.5. Altitude measurement on an actual drone.

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