Flight Dynamics, Stability and Control

What it is about

In this module you will learn the dynamic fundamentals of aircraft: coordinate systems, nonlinear equations of motion, as well as models for aerodynamic forces and propulsion. You will be able to determine steady flight states, analyze static stability and controllability, and compute important indices such as the neutral point, maneuver point, trim rudder deflections, and trim angle of attack.

What you will be able to do

• Calculate neutral point and maneuver point
• Calculate trim rudder deflections and trim angle of attack
• Understand aerodynamic moment derivatives and their influence
• Determine stationary flight states (e.g., straight+level, climb, pull-up, coordinated turn)
• Assess static stability and controllability in longitudinal and lateral dynamics
• Analyze linearized equations of motion and eigenmotions

What the module consists of

• LectureConveying theoretical content and models for flight system dynamics
• Exercises / problem sheetsApplication of lecture content through calculations (e.g., neutral point, trim values)

Teaching method

• Lecture/PresentationIntroduction and explanation of further topics in flight system dynamics
• Problem sheetsPractical exercise and application of methods for calculating stability and trim quantities
• Lecture slides/Formula collectionSupport for self-study and as reference material