Illustrate out the wing and aft tail contribution to the stick fixed static stability.
Discuss the phenomenon of the aileron reversal, adverse yaw, and steps to control adverse yaw and coupling between the rolling and yawing moments.
Quantitavely illustrate contribution of dissimilar components of aircraft towards directional stability and describe directional control.
Illustrate the rigid body equations of the motions of an airplane.
Illustrate out the term stability derivatives. Derive them.