Lesson 16: Basic Control Modes

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Presentation transcript:

Lesson 16: Basic Control Modes ET 438a Automatic Control Systems Technology lesson16et438a.pptx

Learning Objectives After this presentation you will be able to: Describe the common control modes used in analog control systems List the characteristics of common control modes Write the time, Laplace and transfer functions of common control modes Identify the Bode plots of common control modes Design OP AMP circuits that realize theoretical control mode performance. lesson16et438a.pptx

Control Modes-Proportional Control Action Process characteristics for optimum results: 1) Small process capacitance 2) Rapid load changes Limitations: Small steady-state error may require high gain to achieve acceptable error levels Mathematical representations Where: e = time domain error signal Kp = proportional gain vo = controller output with e=0 v = controller time domain output Time function: Laplace function: Note: Initial condition vo=0 on Laplace function Transfer function: lesson16et438a.pptx

Proportional Control Frequency Response Bode plots of three values of Kp: Kp1=0.1, Kp2=1, and Kp3=100 Note: gain is independent of frequency. Kp3 Practical realization: Non-inverting OP AMP circuit Kp2 Kp1 lesson16et438a.pptx

Motor Speed Control Example 16-1: Determine the effect of applying proportional control to the block diagram shown below. The motor produces the following results with the control loop open: TL1 = 0.05 N-m TL2 = 0.075 N-m (50% increase in load) VT = 19.24 Vdc VT=19.24 Ia1 = 1.033 A Ia2 = 1.45 A w1 = 300 rad/sec w2 = 291.7 rad/sec r e + Controller Kp v Power Supply Gamp VT Motor & Load w Tach Generator, Ktac - cm lesson16et438a.pptx

Motor Speed Control Motor Parameters: Tf = 0.012 N-m Ra = 1.2 ohms KT = 0.06 N-m/A Ktac = 0.11 V-sec/rad Ke = 0.06 V-sec/rad KpGamp = 10 V/V Solution: Find the error produced and the setpoint value, r. Then write equations around control loop. r e1 + KpGamp=10 VT = 19.24 V Ktac= 0.11 V-s/rad - cm1 w =300 rad/sec lesson16et438a.pptx

Example 16-1 Solution (2) Combine equations Substitute values Simplify Compute error Substitute values Simplify The initial setpoint value of r=34.924 V with an error of 1.924 V at a speed of 300 rad/s and TL1=0.05 N-m lesson16et438a.pptx

Example 16-1 Solution (3) When torque increase to TL2=0.075 N-m new VT is defined by… Substitute in Tachometer formula Since setpoint, r does not change error must change due to measured speed change. Motor equations Combine these equations to get: Need two equations to find both VT2 and wm2. lesson16et438a.pptx

Example 16-1 Solution (4) Substitute in known values and simplify equation to get first relationship. r1=34.924 V KpGamp=10 Ktac = 0.11 V-s/rad Equation 1 Now use the motor armature circuit equation and the armature current for TL2 =0.075 N-m to find second independent equation. Ia2 =1.45 A Ke = 0.06 V-s/rad R+ =1.2 ohms Equation 2 lesson16et438a.pptx

Example 16-1 Solution (5) Place equations (1) and 2) into standard form and solve simultaneously using software or calculator. Answers Now compute the error signal from the new tachometer output voltage cm2. Error increases e2>e1 1.968>1.924 V to rebalance system lesson16et438a.pptx

Example 16-1 Solution (6) Now determine the percentage speed changes for open loop and feedback control. Setpoint, r=300 rad/sec Open loop speed change Answers Feedback loop speed change Feedback reduces speed error by factor of 19.35 Answers lesson16et438a.pptx

Integral Control Mode Integral Mode characteristics: 1) Output is integral of error over time 2) Drives steady-state error to zero 3) Adds pole to transfer function at s=0 (infinite gain to constant) 4) Integrators tend to make systems less stable Equations Where KI = integral gain constant Time: Laplace: Transfer Function: lesson16et438a.pptx

OP AMP Realizations of Integral Control Practical OP AMP Integrator Ideal OP AMP Integrator Transfer Function Transfer Function One pole at s=0 One pole at s=-1/Rf∙C lesson16et438a.pptx

Bode Plots of Integrator Circuits Substitute jw for s and find the magnitude and phase shift of the transfer function for different values of w. Ideal Integrator Practical Integrator Take magnitude and phase shift of each of these functions using rules of complex numbers. z=a+jb Magnitude of z: z=|z| Phase Shift Scale for dB lesson16et438a.pptx

Bode Plots of Integrator Circuits Practical Integrator Circuit Taking magnitude gives Phase Shift gives 180 degree phase shift is from inverting configurations Ideal Integrator Circuit Magnitude gives Phase shift lesson16et438a.pptx

Integrator Bode Plots Using MatLAB Use MatLAB script to generate Bode plots and transfer function. Define parameters: Ri = 10 kW, Rf = 100 kW, C = 0.01 mF MatLAB Script ri=input('Enter value of input resistance: '); c=input('Enter value of capacitance: '); rf=input('Enter value of feedback resistance: '); % compute transfer function model parameters for % practical integrator tau=rf*c; ki=-rf./ri; Input statement Comments begin with % lesson16et438a.pptx

Integrator Bode Plots Using MatLAB MatLAB Script (Continued) % compute parameter for ideal integrator tau1 = ri*c; % build transfer functions % denominator form is a1*s^2+a2s+a3 Av=tf([ki],[tau 1]) Av1=tf([-1],[tau1 0]) %plot both on the same graphs bode(Av,Av1); Create transfer functions Plot both graphs on same figure lesson16et438a.pptx

Integrator Bode Plots Using MatLAB w=1/RiC w=1000 rad/s lesson16et438a.pptx

Integral Action on Time Varying Error Signals Integral of constant, k, is line with slope k. Integrator produces a linearly increasing output for constant error input e2 e1 e4=0 Negative error causes decreasing output -e3 V(t)=-e3t Zero error maintains last output value V(t)=e2t V(t)=e1t lesson16et438a.pptx

Estimating Integrator Output From Calculus, integral is sum of area below a function plot t f(t) f(ti+1) b a Dt For linear error plots, integral is the sum of the areas of linear segments. Use triangle, trapezoid, and rectangle formulas to approximate output lesson16et438a.pptx

Integrator Output Example 16-2: An ideal integrator has a gain of KI =0.1 V/s. Its initial output is v=1.5 V. Determine the integrator outputs if the error has step increases given by the table below. Error Magnitude (V) Time Interval e(t)=0 0≤t≤1 seconds e(t)=2.5 1<t≤2 seconds e(t)=4 2<t≤3 seconds 3<t≤4 seconds e(t)=-1.5 4<t≤5 seconds lesson16et438a.pptx

Example 16-2 Solution (1) Plot the error function that is input to the integrator lesson16et438a.pptx

Example 16-2 Solution (1) Use the approximate formula to find the error at the end of each interval V0=1.5 A0=KI∙Dt∙e0 =0.1(1)(0) =0 V1=1.5+A0=1.5+0=1.5 A2 A1=KI∙Dt∙e1 =0.1(1)(2.5) =0.25 V2=1.5+A1=1.5+0.25=1.75 A1 A3 A2=KI∙Dt∙e2 =0.1(1)(4) =0.40 V3=1.75+A2=1.75+0.40=2.15 A4 A3=KI∙Dt∙e3 =0.1(1)(0) =0 A0 V4=2.15+A3=2.15+0.0=2.15 A4=KI∙Dt∙e4 =0.1(1)(-1.5) =-0.15 V5=2.15+A4=2.15+-0.15=2.00 lesson16et438a.pptx

Example 16-2 Solution (2) Integrator output plot lesson16et438a.pptx

Derivative Control Mode Derivative Control Characteristics: Produces output only when error is changing Output is proportional to rate of change in error Derivative control never used alone Used with proportional and/or integral modes Anticipates error by observing the rate of change lesson16et438a.pptx

Derivative Mode Equations Time Equation: Laplace Equation: Transfer Function Equation: Differentiators are high-pass filters to sinusoidal signals. They increase sensitivity to rapid error changes when added to controllers. lesson16et438a.pptx

OP AMP Realizations of Differentiators Ideal OP AMP Differentiator Practical OP AMP Differentiator Transfer Function Transfer Function Introduces: zero at s=0 pole at s=-1/Ri∙C Introduces one zero at s=0 lesson16et438a.pptx

Bode Plots of Differentiators Ideal Differentiator Equations Practical Differentiator Equations Use MatLAB script to generate Bode plots and transfer function. Define parameters: Ri = 10 kW, Rf = 100 kW, C = 0.01 mF lesson16et438a.pptx

Bode Plots of Differentiators w=1/RiC lesson16et438a.pptx

End Lesson 16: Basic Control Modes ET 438a Automatic Control Systems Technology End Lesson 16: Basic Control Modes lesson16et438a.pptx