The roll control autopilot of a jet fighter is shown. Assume that the closed-loop complex poles dominate for the system. Select the gain K so that the roll angle has a percent overshoot equal to 16%. What is the resulting peak time? Plot the step response of the Aileron actuator Aircraft dynamics K 12.2 (s) Roll angle s + 7 s(s + 2.2) Part d system. Gyro K = 1

The roll control autopilot of a jet fighter is shown. Assume that the closed-loop complex poles dominate for the system. Select the gain K so that the roll angle has a percent overshoot equal to 16%. What is the resulting peak time? Plot the step response of the Aileron actuator Aircraft dynamics K 12.2 (s) Roll angle s + 7 s(s + 2.2) Part d system. Gyro K = 1

Power System Analysis and Design (MindTap Course List)

6th Edition

ISBN:9781305632134

Author:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma

Publisher:J. Duncan Glover, Thomas Overbye, Mulukutla S. Sarma

Chapter12: Power System Controls

Section: Chapter Questions

Problem 12.1P

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