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Flow Rate Control System

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Presentation on theme: "Flow Rate Control System"— Presentation transcript:

1 Flow Rate Control System
“Root Locus Plotting” March 22, 2006 U.T.C. Engineering 329

2 Yellow Team Jimy George Jeff Lawrence Taylor Murphy Jennifer Potter

3 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

4 Flow System Setup

5 Block Diagram

6 Steady State Operation

7 SSOC

8 Experimental and Model Results
K (lb/min/%) = 0.26 Tau (sec) = 0.46 t0 (sec) = 0.42

9 Frequency Response Experiment

10 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

11 Model Bode Plot K (lb/min/%) = 0.22 t0 (sec) = 0.35 Tau (sec)= 0.25

12 Model Bode Plot K (lb/min/%) = 0.22 t0 (sec) = 0.35 Tau (sec)= 0.25

13 FOPDT Parameters K = 0.24 lb/min/% Tau = 0.28 sec t0 = 0.4 sec

14 Closed Loop Transfer Function

15 Root Locus Theory Use Pade’s Approximation Find Roots of Denominator

16 Root Locus Parameters KCD KQD KCU

17 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

18 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

19 Conclusions (cont.) For: Overdamped Kc needed: 0 < Kc < 0.08
For: Critically Damped Kc needed: Kc = 0.08 *all units are %*min / lb

20 Conclusions (cont.) For: Underdamped Kc needed: 0.08 < Kc < 10
For: Quarter Decay Kc needed: Kc = 6.6 *all units are %*min / lb

21 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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