Outline • PD compensation. • PI compensation. • PID compensation. PD, PI, PID Compensation M. Sami Fadali Professor of Electrical Engineering University of Nevada 1 2 PD Control Remarks = loop gain = desired closed-loop pole location. • Find a controller s.t. or its odd multiple (angle condition). • Controller Angle for • Graphical procedures are no longer needed. • CAD procedure to obtain the design parameters for specified . » evalfr(L,scl) % Evaluate L at scl » polyval( num,scl) % Evaluate num at scl • The complex value and its angle can also be evaluated using any hand calculator. • Zero location 3 4 Procedure:MATLAB or Calculator Procedure 5.2: Given 1. Calculate »theta = pi angle(evalfr(l, scl) ) 2. Calculate zero location using 3. Calculate new loop gain (with zero) » Lc = tf( [1, a],1)*L 4. Calculate gain (magnitude condition) » K = 1/abs( evalfr( Lc, scl)) 5. Check time response of PD-compensated system. Modify the design to meet the desired specifications if necessary (MATLAB). & 1. Obtain error constant from and determine a system parameter that is fixed for the remains free after system with PD control. 2- Rewrite the closed-loop characteristic equation of the PD controlled system as 5 6 Procedure 5.2 (Cont.) Example 5.5 3. Obtain corresponding to the desired closedcan loop pole location. As in Procedure 5.1, be obtained by clicking on the MATLAB root locus plot or applying the magnitude condition using MATLAB or a calculator. 4. Calculate the free parameter from the gain . Use a CAD package to design a PD controller for the type I system 5. Check the time response of the PD compensated system and modify the design to meet the desired specifications if necessary. 7 to meet the following specifications (a) = 0.7 & rad/s. (b) = 0.7 & due to a unit ramp. 8 (a) & (a) Design (cont.) MATLAB Calculate pole location & corresponding gain >> scl = 10*exp( j*( pi-acos(0.7) ) ) scl = 7.0000 + 7.1414I >> g=zpk([ ],[0,-4],1); >> theta=pi( angle( evalfr( g, scl) ) ) theta = 1.1731 » a = 10 * sqrt(1-0.7^2)/ tan(theta) + 7 a= 10.0000 » k =1/abs(evalfr(tf( [1, a],1)*g,scl)) % k= 10.0000 Gain at scl: 9 RL of Uncompensated System Root Locus 8 0.7 0.7 System: gcomp Gain: 10 Pole: -7.01 + 7.13i Damping: 0.701 Overshoot (%): 4.56 Frequency (rad/sec): 10 6 6 4 5 2 Imaginary Axis Imaginary Axis RL of PD-compensated System Root Locus 8 7 10 4 3 10 0 -2 2 -4 1 -6 0 -8 -7 -6 -5 -4 -3 -2 -1 0 -8 -20 Real Axis 11 0.7 -18 -16 -14 -12 -10 Real Axis -8 -6 -4 -2 0 12 (b) for unit ramp L (b) Design (cont.) L → → • Assume that K varies with K a fixed, then • Closed-loop characteristic equation with PD • RL= circle centered at the origin 13 RL of PD-compensated System 14 (b) Design Cont. fixed Desired location: intersection of root locus with radial line. K = 10, a =10 (same values as in Example 5.3). MATLAB command to obtain the gain » k = 1/abs( evalfr( tf([1,10],[ 1, 4, 0]), scl) ) k= 10.0000 • Time responses of two designs are identical. 15 16 PI Control • • • PI Remarks Integral control to improve (increases type by one) worse transient response or instability. Add proportional control controller has a pole and a zero. Transfer function of proportional-plusintegral (PI) controller • Used in cascade compensation (integral term in the feedback path is equivalent to a differentiator in the forward path) • PI design for a plant transfer function is the same as PD design of . • A better design is often possible by "almost canceling" the controller zero and the controller pole (negligible effect on time response). 17 Procedure 5.3 18 Comments 1. Design a proportional controller for the system to meet the transient response specifications, i.e. place the dominant . closed-loop poles at 2. Add a PI controller with the zero location such that (small angle) • Use PI control only if P-control meets the transient response but not the steady-state error specifications. Otherwise, use another control. • Use pole-zero diagram to prove zero location formula. or 3. Tune the gain of the system to moved the closed-loop pole closer to 19 20 Proof Pole-zero Diagram of PI Controller scl j tan 180° d z scl a • From Figure p scl a • Controller angle at n tan 180° 21 22 Controller Angle at Proof (Cont.) • Trig. Identity 3.5 3 2.5 2 1.5 • Solve for • Multiplying by 1 0.5 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 gives 23 24 Solution Example 5.6 • To use the PD procedure for PI design, consider Design a controller for the position control system to perfectly track a ramp input with a dominant pair with . • Procedure 5.1 with modified transfer function. • Unstable for all gains (see root locus plot). • Controller must provide an angle 249 at the desired closed-loop pole location. • Zero at 1.732. 25 RL of System With Integrator • Cursor at desired pole location on compensated system RL gives a gain of about 40.6. 26 RL of PI-compensated System Root Locus 6 5 Imaginary Axis 4 3 0.7 2 1 0 -10 -8 4 -4 -6 Real Axis -2 0 27 28 Analytical Design MATLAB » scl = 4*exp(j*(pi acos( 0.7)) ) scl = -2.8000 + 2.8566i » theta = pi + angle( polyval( [ 1, 10, 0, 0], scl ) ) theta = 1.9285 » a = 4*sqrt(1-.7^2)/tan(theta)+ 4*.7 a= 1.7323 » k = abs(polyval( [ 1, 10, 0,0], scl )/ polyval([1,a], scl) ) k= 40.6400 • Closed-loop characteristic polynomial • Values obtained earlier, approximately. 29 Design I Results Closed-loop transfer function for Design I • Zero close to the closed-loop poles excessive PO (see step response together with the response for a later design: Design II). 31 30 Step Response of PI-compensated System Design I (dotted), Design II (solid). 32 Design II: Procedure 5.3 For zero location Compare Designs I & II rad/s. 7.143 0.7 1 0.49/ tan 3° • Design II dominant poles: 0.5 Closed-loop transfer function rad/s • Time response for Designs I and II • Percentage overshoot for Design II (almost pole-zero cancellation) << Percentage overshoot for Design I (II better) Gain slightly reduced to improve response. 33 PID (proportional-plus-integralplus-derivative) Control 34 PID Design Procedures • Improves both transient & steady-state response. proportional, integral, derivative gain, resp. • Controller zeros: real or complex conjugate. 35 1. Cancel real or complex conjugate LHP poles. 2. Cancel pole closest to (not on) the imaginary axis then add a PD controller by applying Procedures 5.1 or 5.2 to the reduced transfer function with an added pole at the origin. 3. Follow Procedure 5.3 with the proportional control design step modified to PD design. The PD design meets the transient response specifications and PI control is then added to improve the steady-state response. 36 Example 5.7 Design I • Cancel pole at 1 with a zero & add an integrator Design a PID controller for the transfer function to obtain zero due to and rad/s. ramp, • Same as transfer function of Example 5.6 • Add PD control of Example 5.6 • PID controller 37 Design II 38 Design II (Cont.) • Design PD control to meet transient response specs. • Select rad/s (anticipate effect of adding PI). Design PD controller using MATLAB commands » [k,a,scl] = pdcon(0.7, 5, tf(1, [1,11,10,0])) k = 43.0000 a = 2.3256 scl = -3.5000 + 3.5707i 39 • Obtain PI zero (approx. same as ) » b =5 /(0.7 + sqrt(1-.49)/tan(3*pi/ 180) ) % b= 0.3490 Transfer function for Design II (reduce gain to 40 to correct for PI) 40 Time response for Design I(dotted) and Design II (solid) Conclusions • Compare step responses for Designs I and II: Design I is superior because the zeros in Design II result in excessive overshoot. • Plant transfer function favors pole cancellation in this case because the remaining real axis pole is far in the LHP. If the remaining pole is at 3, say, the second design procedure would give better results. • MORAL: No easy solutions in design, only recipes to experiment with until satisfactory results are obtained. 41 Example 5.8 Solution Design a PID controller for the transfer function to obtain zero due to step, and 42 • Complex conjugate pair slows down the time response. • Third pole is far in the LHP. • Cancel the complex conjugate poles with zeros and add an integrator rad/s 43 44 Step Response of PIDcompensated System Solution (cont.) • Stable for all gains. • Closed-loop characteristic polynomial • Equate coefficients with (meets design specs) • PID controller In practice, pole-zero cancellation may not occur but near cancellation is sufficient to obtain a satisfactory time response 45 46