This is ‘lift’ in the downwards direction. In the latter, a negative lift can be produced. In the former case, more lift is produced. ![]() The flight control surfaces work by increasing or decreasing the AOA of the aircraft. This results in a higher pressure difference and therefore, a larger lift force. ![]() The greater the AOA, the greater the airflow separation between the top and bottom of the aerofoil. The angle of attack (AOA) is the angle between the wing chord and the relative wind. The rudder is deflected to the left causing the nose of the aircraft to turn left, while the rudder is deflected to the right causing the nose of the aircraft to turn right.Īircraft Flight Control Systems: The creation of a lift on a positively cambered aerofoil.
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