Aircraft aerodynamic forces and moments can be expressed as a func-
tion of the dynamic pressure, aircraft dimensions and flight conditions. They are
very important do predict the aircraft behavior and performance. Moreover, they
play an important role predicting the model response to control inputs. For these
reasons it is important to accurate determine the aerodynamic characteristics in
terms of stability and control derivatives. This study presents a methodology to
precisely estimate stability and control derivatives through system identification
procedure. Navion FAR 23 airplane model was used for this purpose. A bio-inspired
optimization method was used to create optimal input control signals to excite the
model and obtain an output signal with good frequency content that allowed to
properly identify the system. Inclusion of bio-inspired methods increased the accu-
racy of the estimates. The method can be used to identify fixed wing platforms of
similar characteristics. Results can be used to develop flight simulators to collect
system information regarding certification evidences and to train pilots