The module introduces key techniques and concepts used in the analysis of the trim, stability, and dynamic response characteristics of conventional fixed-wing aircraft.
Also introduced are a several important feedback control design methods, useful for modifying and improving aircraft stability and control characteristics, including Root Locus, Bode and Nyquist based design methods for PID control.
As part of the module, students will undertake a flight test course in the National Flying Laboratory Centre to assess the performance and stability qualities of a real aircraft in flight.