HW12_09 - ” and modify as required After you have...

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AE361 Advanced Stability and Control Homework 12 For the B747 aircraft as described in “ long_stab_B747_inp ”, design a pid controller. As a starting point use the matlab code “ pitch_angle_autopilot_06
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Unformatted text preview: ” and modify as required. After you have designed the controller plot the impulse response and step response and see how it compares with the result obtained using only pitch angle feedback....
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