Question: Assignment # 0 3 Submission due: 1 5 / 1 1 / 2 0 2 4 ; Friday Figure A: Control system of pitch
Assignment# Submission due: ; Friday
Figure A: Control system of pitch angle of an aircraft.
Figure B: Ultimate gain and ultimate period or oscillation period.
Note: Apply the RouthHurwitz criteria to determine the ultimate gain in locating the intersection of the root locus point on the imaginary axis. Then find the ultimate period in Figure B
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