An aircraft aileron can be modeled as a first order system

where p depends on the aircraft. Obtain a family of step responses for the aileron system in the feedback configuration shown in Figure CP12.2.
The nominal value of p = 10. Compute a reasonable value of K so that the step response (with p = 10) has Ts

FIGURE CP12.2 Closed-loop control system for the aircraft aileron.

Transcribed Image Text:

G(s) = 4 s+p Aileron R(s)