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KxM = Jö + bø - co where Ø denotes the angle of attack (output). M is the correction moment (input), K, is the moment gain, J is the moment of inertia along the rotation axis, b is the coefficient of Viscous friction, C is the coefficient of gravitational loading due to offset. J=7400kgm^2c=4670 Nm/rad, b=3550 Nms/rad, Kx =5000 Initial conditions are zero. Design a LEAD-LAG Controller such that the maximum overshoot is 12% and the settling time is 4 seconds and the steady state error is less than 0.3 when we implement unit step as the input. Clearly explain the necessary steps. Use a MATLAB Script for the controller design. Using MATLAB/Simulink, simulate the controller. Use a 2-input scope to plot the output and the step input. Show the Simulink model and its parameters. Make a sketch of the step input and system response Indicate the steady state error.

KxM = Jö + bø - co where Ø denotes the angle of attack (output). M is the correction moment (input), K, is the moment gain, J is the moment of inertia along the rotation axis, b is the coefficient of Viscous friction, C is the coefficient of gravitational loading due to offset. J=7400kgm^2c=4670 Nm/rad, b=3550 Nms/rad, Kx =5000 Initial conditions are zero. Design a LEAD-LAG Controller such that the maximum overshoot is 12% and the settling time is 4 seconds and the steady state error is less than 0.3 when we implement unit step as the input. Clearly explain the necessary steps. Use a MATLAB Script for the controller design. Using MATLAB/Simulink, simulate the controller. Use a 2-input scope to plot the output and the step input. Show the Simulink model and its parameters. Make a sketch of the step input and system response Indicate the steady state error.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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KxM = Jö + bø - co where Ø denotes the angle of attack (output). M is the correction moment (input), K, is the moment gain, J is the moment of inertia along the rotation axis, b is the coefficient of Viscous friction, C is the coefficient of gravitational loading due to offset. J=7400kgm^2c=4670 Nm/rad, b=3550 Nms/rad, Kx =5000 Initial conditions are zero. Design a LEAD-LAG Controller such that the maximum overshoot is 12% and the settling time is 4 seconds and the steady state error is less than 0.3 when we implement unit step as the input. Clearly explain the necessary steps. Use a MATLAB Script for the controller design. Using MATLAB/Simulink, simulate the controller. Use a 2-input scope to plot the output and the step input. Show the Simulink model and its parameters. Make a sketch of the step input and system response Indicate the steady state error.
Transcribed Image Text:KxM = Jö + bø - co where Ø denotes the angle of attack (output). M is the correction moment (input), K, is the moment gain, J is the moment of inertia along the rotation axis, b is the coefficient of Viscous friction, C is the coefficient of gravitational loading due to offset. J=7400kgm^2c=4670 Nm/rad, b=3550 Nms/rad, Kx =5000 Initial conditions are zero. Design a LEAD-LAG Controller such that the maximum overshoot is 12% and the settling time is 4 seconds and the steady state error is less than 0.3 when we implement unit step as the input. Clearly explain the necessary steps. Use a MATLAB Script for the controller design. Using MATLAB/Simulink, simulate the controller. Use a 2-input scope to plot the output and the step input. Show the Simulink model and its parameters. Make a sketch of the step input and system response Indicate the steady state error.
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