- The Transfer Function For An Afti F 16 Aircraft Relating Angle Of Attack A T To Elevator Deflection 8 1 Is Given 1 (63.97 KiB) Viewed 22 times
The transfer function for an AFTI/F-16 aircraft relating angle of attack, a(t), to elevator deflection, 8.(1), is given
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The transfer function for an AFTI/F-16 aircraft relating angle of attack, a(t), to elevator deflection, 8.(1), is given
The transfer function for an AFTI/F-16 aircraft relating angle of attack, a(t), to elevator deflection, 8.(1), is given by ii) Assume the block diagram shown in Figure Q4 for controlling the angle of attack, a and 5 do the following i) iii) (s+23) (s² +0.05s+0.04) (s-7)(s+1.7) (s² +0.08s +0.04) a(s) G(s)= = 0.072- 8, (s) Find the range of K for stability. Plot or sketch a root locus. [5 Marks] [CO2, PO2, C3] [10 Marks] [CO3, PO3, C4] Design a cascade compensator to yield zero steady-state error, a settling time of about 0.05 second, and a percent overshoot not greater than 20%.