Aerospace, Defense and Mechanical Engineering

Aircraft Stability and Control

The ability of an aircraft to maintain its desired flight attitude in the air is known as aircraft stability. The ability to alter an aircraft's attitude and flight direction is the subject of aircraft control. During the preliminary design phase, it is necessary to investigate both of these concerns .In other words, civil aircraft are not specifically designed to provide stability and control as design criteria. They were created to perform. After developing a preliminary design that satisfies the performance requirements, its stability is evaluated, and its control is designed.