Aircraft flight dynamics and control

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Module Description

Padfield, Gareth D. Sadraey, Mohammad H.

Forrester, Alexander I J. Aircraft Flight Dynamics and Control addresses airplane flight dynamics and control in a largely classical manner, but with references to modern treatment throughout. Short period oscillation. Response calculations.

Flight Dynamics and Control: Lecture 3, First steps at deriving aircraft equations of motion

Definitions of natural and damped oscillation frequencies,damping index, relative damping ratio, period of oscillation. Simple Lateral Motion : Rudder and aileron controls, forces and moments produced. Introduction to the concept of aerodynamic derivatives. Lateral static stability.

Flight Dynamics, Simulation, and Control: For Rigid and Flexible Aircraft

Trim med lateral manoeuvres: correctly banked turn, steady straight sideslip and minimum control speeds. Introduction to lateral dynamics. Lateral stability modes: roll, spiral and dutch roll modes. Examples of simple response calculations.

Aircraft-Flight Mechanics and Controls | Mechanical and aerospace

Equations of Motion for a Rigid Aircraft: Derivation of the non-linear equations of motion in six degrees of freedom. Notation and sign conventions. Axes systems. Longitudinal and lateral motions: linearisation of the equations of motion. Introduction to aerodynamic derivatives: non-dimensional, normalised, concise aerodynamic derivatives.

Longitudinal Aerodynamic Derivatives : Force velocity and pitching moment derivatives. Derivatives due to rate of pitch. Control derivatives. Lateral Aerodynamic Derivatives : Derivatives due to: sideslip, rate of roll, rate of yaw. Examples of such complex behavior include the phenomena of surge and stall of compressors used in jet engines, wing rock oscillations and jump phenomena in combat aircraft, and structural vibrations in flexible space structures.

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These complex phenomena require equally complex control strategies to meet the stringent performance requirements on aerospace systems. The dynamical behavior of aerospace systems as well as the control strategies that it warrants present a challenge to the analysis and design of aerospace control systems.

Techniques based on bifurcation theory, nonlinear dynamical systems theory, linear and nonlinear control theory, stability theory, and neural and fuzzy control are being developed and applied to problems in aircraft flight dynamics and control, combustion acoustics, spacecraft attitude dynamics and control, and control of structural vibrations.