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

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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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This note was uploaded on 01/11/2011 for the course MECH ENG AE361 taught by Professor Waltereversman during the Fall '10 term at Missouri S&T.

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