9. A fighter aircraft has the transfer function ė -10(s+1)(5 +0.01) 8 (²+25+2)(s² +0.02s +0.0101) where is the pitch rat

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9 A Fighter Aircraft Has The Transfer Function E 10 S 1 5 0 01 8 25 2 S 0 02s 0 0101 Where Is The Pitch Rat 1 (37.63 KiB) Viewed 35 times

9. A fighter aircraft has the transfer function ė -10(s+1)(5 +0.01) 8 (²+25+2)(s² +0.02s +0.0101) where is the pitch rate (rad/sec) and is the elevator deflection (rad). The four poles represent the phugoid and short-period modes. The phugoid mode has a natural frequency of 0.1 rad/sec, and the short period mode is 1.4 rad's. The block diagram is shown in Figure Q9. a) Let the lead compensator be G₁(s) = KS+z s+p where <p Using MATLAB and Bode plot methods, design the lead compensator to meet the following specifications: 1. 11. comm 111. R(s) Settling time to a unit step less than 2 second. Percent overshoot less than 10% Simulate the closed loop system with a step input of 10°/second. and show the time history of K₁ +K₂s Figure Q9 1 Js C(s)