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Flow Rate Control System
“Root Locus Plotting” March 22, 2006 U.T.C. Engineering 329
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Yellow Team Jimy George Jeff Lawrence Taylor Murphy Jennifer Potter
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Outline Flow System Background Previous Work Root Locus Theory
Modeling Results Conclusions First, I will provide a brief background in the Level II System Followed by FOPDT Theory & Model Theory Then I will discuss our results and colclude the presentation
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Flow System Setup
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Block Diagram
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Steady State Operation
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SSOC
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Experimental and Model Results
K (lb/min/%) = 0.26 Tau (sec) = 0.46 t0 (sec) = 0.42
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Frequency Response Experiment
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Bode Plots Kcu (%*min/lb) = 10.00 K (lb/min/%) = 0.24 Tau (sec) = 0.27
t0 (sec) = 0.35 m (order) = 1.14 fu (Hz) = 0.95 Bode Plots
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Model Bode Plot K (lb/min/%) = 0.22 t0 (sec) = 0.35 Tau (sec)= 0.25
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Model Bode Plot K (lb/min/%) = 0.22 t0 (sec) = 0.35 Tau (sec)= 0.25
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FOPDT Parameters K = 0.24 lb/min/% Tau = 0.28 sec t0 = 0.4 sec
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Closed Loop Transfer Function
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Root Locus Theory Use Pade’s Approximation Find Roots of Denominator
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Root Locus Parameters KCD KQD KCU
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Response to Step Change in Set Point
Symbol Average Critical Damping KCD 0.08 1/500th Decay KC500 1.8 1/10 Decay KC10 4.8 Quarter Decay KQD 6.6 Ultimate KCU 10 ζ Locations
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Results From Root Locus
Ultimate Quarter Decay Critically Damped Underdamped Overdamped Kc = 10 Kc = 6.6 Kc = 0.08 0.08 < Kc < 10 0 < Kc < 0.08 *all units are %*min / lb
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Conclusions (cont.) For: Overdamped Kc needed: 0 < Kc < 0.08
For: Critically Damped Kc needed: Kc = 0.08 *all units are %*min / lb
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Conclusions (cont.) For: Underdamped Kc needed: 0.08 < Kc < 10
For: Quarter Decay Kc needed: Kc = 6.6 *all units are %*min / lb
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Response to Step Change in Set Point
Conclusions (cont.) Response to Step Change in Set Point KC (%*min/lb) Offset (lb/min) Critical Damping 0.08 4.9 1/500th Decay 1.8 3.5 1/10 Decay 4.8 2.3 Quarter Decay 6.6 1.9 Ultimate 10 1.5
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