Specifications

10 Design Case Studies
10-8
The new figure is shown below.
The aircraft is oscillating around a nonzero bank angle. Thus, the aircraft is
turning in response to an aileron impulse. This behavior will prove important
later in this case study.
Typically, yaw dampers are designed using the yaw rate as sensed output and
the rudder as control input. Look at the corresponding frequency response.
sys11=sys('yaw','rudder') % Select I/O pair.