Flight dynamics principles /

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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...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Cook, M. V.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Amsterdam ; Boston : Elsevier/Butterworth-Heinemann, 2007.
Edición:2nd ed.
Colección:Elsevier aerospace engineering series.
Temas:
Aerodynamics.
Flight control.
Stability of airplanes.
Aérodynamique.
Systèmes de commande (Vol)
Avions > Stabilité.
aerodynamics.
TRANSPORTATION > Aviation > General.
Aerodynamics
Flight control
Stability of airplanes
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Flight Dynamics Principles
  • Copyright page
  • Preface to the first edition
  • Preface to the second edition
  • Nomenclature
  • 1. Introduction
  • 1.1. Overview
  • 1.2. Flying and handling qualities
  • 1.3. General considerations
  • 1.4. Aircraft equations of motion
  • 1.5. Aerodynamics
  • 1.6. Computers
  • 1.7. Summary
  • 2. Systems of axes and notation
  • 2.1. Earth axes
  • 2.2. Aircraft body fixed axes
  • 2.3. Euler angles and aircraft attitude
  • 2.4. Axes transformations
  • 2.5. Aircraft reference geometry
  • 2.6. Controls notation
  • 2.7. Aerodynamic reference centres
  • 5.1. Methods of solution
  • 5.2. Cramer's rule
  • 5.3. Aircraft response transfer functions
  • 5.4. Response to controls
  • 5.5. Acceleration response transfer functions
  • 5.6. The state space method
  • 5.7. State space model augmentation
  • Problems
  • 6. Longitudinal dynamics
  • 6.1. Response to controls
  • 6.2. The dynamic stability modes
  • 6.3. Reduced order models
  • 6.4. Frequency response
  • 6.5. Flying and handling qualities
  • 6.6. Mode excitation
  • Problems
  • 7. Lateral-directional dynamics
  • 7.1. Response to controls
  • 7.2. The dynamic stability modes
  • 7.3. Reduced order models
  • 7.4. Frequency response
  • 7.5. Flying and handling qualities
  • 7.6. Mode excitation
  • Problems
  • 8. Manoeuvrability
  • 8.1. Introduction
  • 8.2. The steady pull-up manoeuvre
  • 8.3. The pitching moment equation
  • 8.4. Longitudinal manoeuvre stability
  • 8.5. Aircraft dynamics and manoeuvrability
  • 9. Stability
  • 9.1. Introduction
  • 9.2. The characteristic equation
  • 9.3. The Routh-Hurwitz stability criterion
  • 9.4. The stability quartic
  • 9.5. Graphical interpretation of stability
  • Problems
  • 10. Flying and handling qualities
  • 10.1. Introduction
  • 10.2. Short term dynamic models
  • 10.3. Flying qualities requirements
  • 10.4. Aircraft role
  • 10.5. Pilot opinion rating
  • 10.6. Longitudinal flying qualities requirements
  • 10.7. Control anticipation parameter
  • 10.8. Lateral-directional flying qualities requirements
  • 10.9. Flying qualities requirements on the s-plane
  • Problems
  • 11. Stability augmentation
  • 11.1. Introduction
  • 11.2. Augmentation system design
  • 11.3. Closed loop system analysis
  • 11.4. The root locus plot
  • 11.5. Longitudinal stability augmentation
  • 11.6. Lateral-directional stability augmentation
  • 11.7. The pole placement method.

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