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In the radar tracking system seen in Figure 5, monitor the target aircraft within the framework of requirements (0 (t), 0 (t)’it should be able to follow we are required to design the system a) draw the root location curves of the system. b) the following is required for the commanding step 0 ( t ), which is the step entry: - For rapid response, the system is required to be critical or less damped. -Maximum stationary time should be 4 sec (2% criterion)) maximum overshoot should be 4.32%. Find the gain range that can meet these requirements. Radan receiver Amplifier Motor (a) Plant Motor, pedestal,Da and so forth etr) Power amplifier (b) Power amplifier Plant 1 sis+ 2) (c)

In the radar tracking system seen in Figure 5, monitor the target aircraft within the framework of requirements (0 (t), 0 (t)’it should be able to follow we are required to design the system a) draw the root location curves of the system. b) the following is required for the commanding step 0 ( t ), which is the step entry: - For rapid response, the system is required to be critical or less damped. -Maximum stationary time should be 4 sec (2% criterion)) maximum overshoot should be 4.32%. Find the gain range that can meet these requirements. Radan receiver Amplifier Motor (a) Plant Motor, pedestal,Da and so forth etr) Power amplifier (b) Power amplifier Plant 1 sis+ 2) (c)

Introductory Circuit Analysis (13th Edition)
Introductory Circuit Analysis (13th Edition)
13th Edition
ISBN:9780133923605
Author:Robert L. Boylestad
Publisher:Robert L. Boylestad
Chapter1: Introduction
Section: Chapter Questions
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In the radar tracking system seen in Figure 5, monitor the target aircraft within the framework of requirements (0 (t), 0 (t)’it should be able to follow we are required to design the system a) draw the root location curves of the system. b) the following is required for the commanding step 0 ( t ), which is the step entry: - For rapid response, the system is required to be critical or less damped. -Maximum stationary time should be 4 sec (2% criterion)) maximum overshoot should be 4.32%. Find the gain range that can meet these requirements. Radar receiver ale) Amplifier Motor (a) Plant Motor, pedestal, Oa) and so forth elt) Power amplifier Balt) + (b) Power amplifier Plant sis + 2) (c)
Transcribed Image Text:In the radar tracking system seen in Figure 5, monitor the target aircraft within the framework of requirements (0 (t), 0 (t)’it should be able to follow we are required to design the system a) draw the root location curves of the system. b) the following is required for the commanding step 0 ( t ), which is the step entry: - For rapid response, the system is required to be critical or less damped. -Maximum stationary time should be 4 sec (2% criterion)) maximum overshoot should be 4.32%. Find the gain range that can meet these requirements. Radar receiver ale) Amplifier Motor (a) Plant Motor, pedestal, Oa) and so forth elt) Power amplifier Balt) + (b) Power amplifier Plant sis + 2) (c)
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