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Flight Dynamics and Control

Course Description: Introduction to Aerodynamics, Static and Dynamic Stability, Aircraft Equations of Motion, Response to Control Inputs, Flight Characteristics, Applications of Classical and Modern Control Theories in Autopilot Design.
Credit hours: 3
Objectives of the course :

• Derivation and formulation of flight motion equations: longitudinal and lateral.
• Define the response of aircraft to controls or inputs.
Design, integrate, and troubleshoot flight dynamics and control problems using classical and modern automatic control theory.
Applying numerical techniques to solve flight dynamics and control problems using MATLAB.

Course outputs :
  • Understanding the Concepts of Static and Dynamic Stability.
  • Explanation of the effect of each aircraft component on its static stability.
  • Determination of the static and dynamic stability of an aircraft.
  • Derivation and formulation of flight dynamics equations, longitudinal and lateral motion, and response to control or inputs.
  • Design, integrate, and troubleshoot flight dynamics and control problems using classical and modern control theory.
  • Application of Numerical Techniques for Solving Flight Dynamics and Control Problems Using Matlab.
  • Communicating in various forms to disseminate knowledge, skills, research findings, and innovations.
  • Related to flight dynamics and control.
  • Teamwork, time management.
Additional information:
  • Last updated: 2026-05-17

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