Aircraft Bank Angle Control System - Inner Loop - Engineering Assignment Help

Assignment Task :

1. Figure 1.1 below shows an aircraft bank angle control system which forms the inner loop of the direction control system whose block diagram is shown in figure 1.2.

a) From the plot shown in figure 1.3, which controller gain provides the best response in  terms of stability and speed of response taken together? 

b) Derive the transfer function φ(s)/φc(s) from the block diagram of figure 1.1.  

c) Derive the overall transfer function ψ(s)/ψcom(s) taking g = 9.81 m/s2 and U0 = 150 m/s.   

d) Using the Routh Hurwitz criterion find the maximum value which Kp can take before the  direction control system becomes unstable.

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