CONTROL SYSTEMS. Chapter 5 : Root Locus Diagram. GATE Objective & Numerical Type Solutions. The transfer function of a closed loop system is

Size: px
Start display at page:

Download "CONTROL SYSTEMS. Chapter 5 : Root Locus Diagram. GATE Objective & Numerical Type Solutions. The transfer function of a closed loop system is"

Transcription

1 CONTROL SYSTEMS Chapter 5 : Root Locu Diagram GATE Objective & Numerical Type Solution Quetion 1 [Work Book] [GATE EC 199 IISc-Bangalore : Mark] The tranfer function of a cloed loop ytem i T () where i the path gain. The root locu plot of the ytem i ( ) 1 (A) j (B) = j = = 1 = (C) j (D) j An. (B) Sol. Given : T () ( ) 1 T () Tranfer function for poitive feedback i given by, G () T () 1 GH ( ) ( ) On comparing equation (i) and (ii), we get G ( ), 1 H ( ) Characteritic equation i 1 (i) (ii) 1

2 94 Pole at.81,.618 (iii) Both pole lie at negative real axi. Locate the open loop pole and zero on the -plane, and any point on the real axi i part of root locu if the total number of open loop pole and zero to the right of the point i even (complimentary root locu). j CRL CRL Fig. Pole-zero diagram The characteritic equation i given by, 1 G( ) H ( ) (iv) Breakaway/break-in point can be calculated a, d d d ( ) ( 1) d d 1 d 1 1 From equation (iv), we get ( 1) ( 1) (v) The root locu branch croe the imaginary axi i determined by applying Routh Hurwitz criterion to the characteritic equation. Routh Tabulation : Row of zero 1 = 1, valid breakaway point j The interection of root locu plot with imaginary axi i given by the value of obtained by olving the following equation. (vi) = 1, valid break-in point

3 By uing equation (iii), (v) and (vi) option (B) i atified. = j = 1 = = = Hence, the correct option i (B). Quetion [Work Book] [GATE EE 1991 IIT-Madra : 1 Mark] ( a) A unity feedback ytem ha an open loop tranfer function of the form G() ; b a which ( b) of the loci hown in figure can be valid root-loci for the ytem? (A) (B) j j b a b a (C) j (D) j b a b a An. (A, C) Sol. Number of open loop pole P = at =, and b. Number of open loop zero Z = 1 at = a. The interection point of aymptote on the real axi i called centroid. Centroid i given by, Real partof polein GH ( ) ( ) Real partof zeroin GH ( ) ( ) P Z b a ( b a).. (i) 1 Angle of aymptote : (1) 18 A where,, 1,,... ( P Z 1) P Z If PZ, 1 A 9, 7

4 Now conider two cae. Cae I : 4 a and b = 1 4 ( a) G( ) ( b) ( 1) A point on the real axi lie on the root locu if the um of the number of open loop pole and the open loop zero on the real axi to the right hand ide of thi point i odd. j RL 1 4/ Fig. Pole-zero diagram From equation (i), σ 5. Breakaway/Break-in point can be calculated a, d d Characteritic equation i given by, 1 G( ) H ( ) 4 1 ( 1) ( 1) ( 1 ) 4 4 d d ( 8 16) ( 4) =, 4, 4 There are repeated pole at origin o there i a breakaway point at origin. 4

5 ( ) 18 For = 4, So, = 4 i alo a valid breakaway point. j /, Cae II : a =, b = 4 G( ) = 4 breakaway point ( ) ( 4) A point on the real axi lie on the root locu if the um of the number of open loop pole and the open loop zero on the real axi to the right hand ide of thi point i odd. j RL 4 Fig. Pole-zero diagram ( ba) (4) From equation (i), 1 Breakaway/Break-in point can be calculated a, d d Characteritic equation i given by, 1 GH ( ) ( ) ( 4) ( 4 ) ( ) ( ) d ( )( 8 ) ( 4 ) d ( ) ( 116),.5 j1. For exitence of complex breakaway/break-in point it mut atify angle criteria. 5

6 At.5 j1., (.5 j1.) G() (.5 j1.) (.5 j1. 4) By uing calculator, G( ) = (Not an odd multiple of 18 ) It doe not atify angle criterion. Hence, thi i not a valid breakaway point. j 4 1, Hence, the correct option are (A) and (C) both. Quetion 7 [Practice Book] Sol. [GATE IN 199 IIT-anpur : Mark] A unity feedback ytem ha open loop pole ( j ) and. It ha a ingle zero at ( 4 j). The angle of departure in degree of the root locu branch tarting from the pole ( j ) i. Figure to calculate angle of departure i hown in below. ( j) P j j Pole Zero p1 4 Z 1 z1 P 1 p Angle of departure at complex pole : The angle of departure from an open loop complex pole i given by (for ) d 18 ( pz ) z : Sum of all the angle ubtended by zero. p: Sum of all the angle ubtended by remaining pole. At pole ( j), 1 p 1 18 tan 15 p 9 1 z 1 tan 45 p p 1 p P ( j) j 6

7 z z1 45 d 18 (5 45 ) At pole ( j), d Hence, the anwer i. Quetion 14 [Practice Book] [GATE EE IISc-Bangalore : 5 Mark] ( ) The open loop tranfer function of a unity feedback ytem i given byg (). Sketch ( )( 1) the root locu a varie from to. Find the angle and real axi intercept of the aymptote, breakaway point and the imaginary axi croing point, if any. ( ) Sol. Given : G (), H () 1 ( )( 1) Characteritic equation i given by, 1 G( ) H ( ) ( ) 1 ( )( 1) ( 1) 1 (i) ( 1 ) Modified characteritic equation i given by, 1 G'( ) H '( ) (ii) On comparing equation (i) and (ii), we get G'( ) H'( ) ( 1 ) G '( ) H '( ) 1 1 ( 1 ) 1 1 Concept of root contour : Number of pole, P = at,.6, Number of zero, Z =. j RL 1 RL Fig. Pole-zero diagram 7

8 Number of aymptote, P Z The interection point of aymptote on the real axi i called centroid. Centroid i given by, Realpartof polein G'( ) H'( ) Realpartof zeroin G'( ) H'( ) P Z ( ) 4 An. Angle of aymptote : (1) 18 A where,, 1,,... ( P Z 1) P Z If PZ, 1, Angle of aymptote are Breakaway/break-in point can be calculated a, d d A 6, 18, 6, 18,. An. d 1 d 4 1.6, 6.94 = 6.94 invalid Breakaway point j 1 Rejecting 6.94 a it doen t lie on root locu. Hence, valid break away point 1.6. An. The root locu branch croe the imaginary axi i determined by applying Routh Hurwitz criterion to the characteritic equation. Characteritic equation i given by, 1 G '( ) H '( ) = 1.6 valid Breakaway point 64 1 Row of zero The interection of root locu plot with imaginary axi i given by the value of obtained by olving the following equation. 8

9 Auxiliary equation i formed uing row, j4.69 The root contour diagram i hown in below figure. 1 1 j = j4.69 j4.69 An. Quetion 7 [Practice Book] [GATE EC 9 IIT-Roorkee : Mark] The feedback configuration and the pole-zero location of G( ) are hown below. The root locu for negative value i.e. for, ha breakaway/break-in point and angle of departure at pole P (with repect to the poitive real axi) equal to j G () P An. (A) and (B) and 45 (C) and (D) and 45 (B) Sol. Given : G () j G () P Root locu for negative value of repreent the invere root locu. The characteritic equation i given by, 1 G( ) H( ) 9

10 1 Breakaway/break-in point can be calculated a, d 1 45 j j 1 9 d ( )() ( )() ( ) j P 4 8 Angle of departure for a complex pole 1 j i given by, d ( z p ) Invere root locu where p um of all the angle ubtended by remaining pole z um of all the angle ubtended by zero ( 45 ) ( 9 ) 45 Hence, the correct option i (B). d Note : In the original GATE quetion paper function wa G (). Thi function ha a zero in right half of -plane and pole in left half of -plane but in pole-zero diagram of G( ) the pole are given in the right half and zero in left half of -plane. To correct the quetion function G( ) ha been modified to G (). Quetion 8 [Work Book] [GATE IN 9 IIT-Roorkee : Mark] A unity feedback ytem ha the tranfer function ( b) ( ) The value of b for which the loci of all the three root of the cloed loop characteritic equation meet at a ingle point i (A) 1 (B) (C) (D) An. (B) ( b) Sol. Given : G () ( ) Characteritic equation i given by, 1 G( ) 1

11 ( b) 1 ( ) ( ) ( b) ( ) ( b) d d ( b)( 4 ) ( )(1) ( ) b b 4 4b (b ) 4b [ (b ) 4 b] and (b ) 4b There i repeated pole at origin o there i a breakaway point in origin i.e.. Solving quadratic equation, we get ( b) ( b) b ( b) 4 1b9b b 4 4 ( b) b b ( b) ( b) b 9 4 Cae - I : When b. 9 Breakaway point, Cae - II : When b = 6.67 valid breakaway point Breakaway point, [Not valid] 4 The loci of all thee root can meet at a ingle point only if the breakaway point exit between b. When b. the breakaway point exit at 6.66 which lie between 9 b. In uch cae the open loop tranfer function of the ytem become a under, 9 GH () () ( ) The interection point of aymptote on the real axi i called centroid. 9 j 11

12 Centroid i given by, Real part of pole in GH ( ) ( ) Real part of zero in GH ( ) ( ) P Z σ The number of aymptote, NZ 1 Angle of aymptote : (1) 18 A P Z If P Z, 1 The root locu of the ytem i hown in below figure. where,, 1,,... ( P Z 1) j A 9, 7 /9, Hence, the correct option i (B). Quetion 1 [Practice Book] An. Sol. [GATE IN 1 IIT-Delhi : Mark] The open loop tranfer function of a unity negative feedback control ytem i given by 48 G (). The angle θ, at which the root locu approache the zero of the ytem, atifie ( )( 8) (A) (C) (D) tan tan 4 Open loop tranfer function of a unity feedback ytem i 48 GH () () ( )( 8) (B) (D) 4 4 j j Number of open loop pole, P = at =, and 8. Number of open loop zero, Z = at = + j and j. Pole-zero pattern i hown below. = 6.67 breakaway point tan 1 1 tan 4 1

13 A j j B p1 p p 8 C D z1 j Angle of arrival at complex zero : The angle of arrival for an open loop complex zero i given by (for ) a 18 ( pz ) z : Sum of all the angle ubtended by remaining zero. p: Sum of all the angle ubtended by pole. At j, 1 p 1 tan 4 4 p tan p z1 1 AC BC tan 1 tan p p 1p p tan rad z z1 11 a 18 tan 4 rad a tan tan tan rad rad rad a tan tan 4 rad 4 rad j 1 1 a tan 4 rad 7 (CCW) 4 4 (CW) Hence, the correct option i (D). 1

14 Quetion 1 [Work Book] [GATE EC 14 (Set ) IIT-haragpur : Mark] In the root locu plot hown in the figure, the pole/zero mark and the arrow have been removed. Which one of the following tranfer function ha thi root locu? j 1 (A) 1 ( )( 4)( 7) (B) 4 ( 1)( )( 7) (C) 7 ( 1)( )( 4) (D) ( 1)( ) ( 7)( 4) An. Sol. (B) The given root locu plot i hown below. j 1 For option (A), (B) and (C) : Since P > Z branche will tart from each of the location of open loop pole and terminate at the location of zero. The remaining P Z branche will approach to infinity. Angle of aymptote : (1) 18 A where,, 1,,... ( P Z 1) P Z If PZ, 1 A 9, 7 It mean that root locu branche will approach to infinity with angle The interection point of aymptote on the real axi i called centroid. Centroid i given by, For option (A), 9 and 7. Real partof polein GH ( ) ( ) Real partof zeroin GH ( ) ( ) P Z The root locu for option (A) can be drawn a hown below. 14

15 j Fig. (A) 174 For option (B), 1 The root locu for option (B) can be drawn a hown below. j Fig. (B) 147 For option (C), 1 The root locu for option (C) can be drawn a hown below. j Fig. (C) 741 For option (D), The root locu for option (D) can be drawn a hown below. j Hence, the correct option i (B). Fig. (D) 15

16 Quetion 1 [Work Book] [GATE EC 14 (Set 4) IIT-haragpur : Mark] The characteritic equation of a unity negative feedback ytem i 1 G( ). The open loop tranfer function G( ) ha one pole at and two pole at 1. The root locu of the ytem for varying i hown in the figure. j.5 A 1 1 (, ) O The contant damping ratio line, for.5, interect the root locu at point A. The ditance from the origin to point A i given a.5. The value of at point A i. An.. to.41 Sol. The given root locu for varying i hown below. j.5 A, 1 1 X O Given : GH () (),.5, OA =.5. ( 1) We know that, In AXO, co θ co 6 OX OA OX OAco

17 in θ AX AO AX AO in So, the coordinate of A i 1 j. 4 4 We know that the co-ordinate of point A of the given root locu i.e. magnitude condition. GH () () 1 Applying magnitude condition at GH () () ( 1) 1 j 4 4, we get GH () () 1 1 j j GH () () 1 1 j Hence, the anwer i.75. Alternatively : Graphical calculation of : j 1 j j A P 1 X.5 O From figure, AP (.75) (.4)

18 and OA.5 Hence, the anwer i.75. Quetion [Work Book] Product of vector lengthdrawn from thepoleof GH ( ) ( ) to A Product of vector lengthdrawn from thezeroof GH ( ) ( ) to A The open-loop tranfer function of a unity feedback configuration i given a value of a gain ( ) for which 1 j lie on the root locu i. An. (5.54) Sol. Pole-zero diagram i hown below. P [GATE EC 15 (Set-1) IIT-anpur : Mark] j j G( ) ( 4) ( 8)( 9). The A B C D Vector Length : AP (7) () 5 BP () () 1 CP () () 8 DP (4) () Product of vector lengthdrawn from thepoleof GH ( ) ( ) to P Product of vector lengthdrawn from thezeroof GH ( ) ( ) to P Hence, the correct option i 5.5. Alternatively, By magnitude criteria, GH () () 1 G( ) 1 j 1 j j 7j j 4j Hence, the correct option i 5.5. ( 1 j) 4 ( 1 j) 8 ( 1 j)

19 Quetion [Practice Book] [GATE EE 15 (Set-1) IIT-anpur : Mark] The open loop pole of a third order unity feedback ytem are at, 1,. Let the frequency correponding to the point where the root locu of the ytem tranit to untable region be. Now uppoe we introduce a zero in the open loop tranfer function at, while keeping all the earlier open loop pole intact. Which one of the following i TRUE about the point where the root locu of the modified ytem tranit to untable region? (A) It correpond to a frequency greater than. (B) It correpond to a frequency le than. (C) It correpond to a frequency. (D) Root locu of modified ytem never tranit to untable region. An. (D) Sol. Given : Number of open loop pole, P = at =, 1 and. Open loop tranfer function will be, GH () () ( 1)( ) Root locu plot i hown in figure (a). j 1 Fig. (a) After introducing a zero in open loop tranfer function, ( ) G'( ) H'( ) ( 1)( ) Root locu plot i hown in figure (b). j 1 Fig. (b) From the above figure (b), it can be een that root locu plot never croe j-axi for all value of. Alternatively : The root locu branch croe the imaginary axi i determined by applying Routh Hurwitz criterion to the characteritic equation. Characteritic equation i given by, ( ) 19

20 Routh Tabulation : For ytem to be table > i.e. for all value of ytem i table. Effect of addition of open loop zero in Root Locu (i) Root locu hift to left away from the imaginary axi. (ii) Relative tability of the ytem increae. Hence, the correct option i (D). Quetion 5 [Practice Book] An. [GATE EE 16 (Set-) IISc-Bangalore : Mark] The gain at the breakaway point of the root locu of a unity feedback ytem with open loop tranfer G( ) function ( 1)( 4) i (A) 1 (B) (C) 5 (D) 9 (A) Sol. Given : G () ( 1)( 4) img R- L R- L 1 4 Real Characteritic equation 1 ( 1)( ) ( 1)( 4) For break away point dk d ( 5 4) ( )(5) ( 54)(1) 5 54

21 4 will be valid breakaway point 1 A it lie between two pole. Hence the correct option i (A) IES Objective Solution Quetion 14 [Practice Book] [IES EE ] Identify the correct root locu from the figure given below referring to pole and zero at j8 and j1 repectively of G( ) H( of ) a ingle-loop control ytem. j j (A) (B) j j (C) (D) An. (B) Sol. Given : The ytem ha pole at j8 and zero at j1. Hence, the tranfer function can be written a ( 1) GH () () ( 64) Pole zero location are hown in figure below, j j1 j8 Angle of departure at pole at j8 d1 18 Where, z p j8 j1 1

22 p p1 9 z z 1z d1 18 ( 9 ) 9 d at pole at 8 d 9 j Hence, the root locu i hown below, in which branche of root locu are tarting from pole and are terminating on zero. j d1 9 ACW CW d 9 Hence, the correct option i (B). Quetion 19 [Practice Book] [IES EE 4] A control ytem ha G( ) H ( ) ( ). What i the number of breakaway ( 4)( 4 ) point in the root locu diagram? (A) One (B) Two (C) Three (D) Zero An. (C) Sol. Given : G( ) H ( ) ( ) ( 4)( 4 ) Characteritic equation i given by, 1 G( ) H ( ) 1 ( 4)( 4) ( ) Breakaway point can be calculated a, d d d ( ) d Breakaway point i and two complex breakaway point are j.45. Exitence of complex breakaway point can be calculated uing angle condition. Angle condition :

23 GH n n () () ( 1)18,1,... GH () () ( j.45) ( j.45) 4 ( j.45) 4( j.45) GH () () 18 [Multiple of So j.45 are the valid breakaway point. At, 64 [poitive] So i alo a valid breakaway point. j j ] 4 = valid breakaway point j.45 The number of breakaway point in the root locu diagram i three. The root locu plot i hown in below figure. = + j.45 valid breakaway point j j.45 4 = valid breakaway point j.45 Hence, the correct option i (C). Quetion 4 [Practice Book] [IES EC 1] If the gain of the ytem i reduced to zero value, the root of the ytem in the -plane (A) Coincide with zero (B) Move away from the zero (C) Move away from the pole (D) Coincide with the pole An. (D) Sol. Let u aume G () ( a) and a are open loop pole Characteritic equation i a = j.45 valid breakaway point

24 Root of characteritic equation are, 1 a a When =, the root are 1 and a i.e. they coincide with the open loop pole of ytem. Hence, the correct option i (D). Alternatively : Root locu tart with open loop tranfer function pole where = and terminate to zero where. Quetion 41 [Practice Book] [IES EC 11] Given the root locu of ytem G ().77? 4 1 what will be the gain for obtaining the damping ratio j 1 An. (A) 1 4 (B) Sol. Given : G () (B) and 1 (C) 4 (D) 11 4 Number of open loop pole, P = at = 1 and. Number of open loop zero, Z =. The interection point of aymptote on the real axi i called centroid. Centroid i given by, real part of pole of GH ( ) ( ) real part of zero of GH ( ) ( ) P Z 1 Characteritic equation i given by, 1 G( ) 4 1 ( 1)( ) 4 4.(i) For econd-order ytem, characteritic equation i given by,.(ii) n n 4

25 On comparing equation (i) and (ii), we get n 4 n n 8 n 4 n Hence, the correct option i (B). Alternatively : Graphical analyi of : B j 5 C A 45 D co 45 1 AB tan 45 1 OA AB OA CB 1 5 BD 1 5 Product of vector lengthdrawn from the poleof GH ( ) ( ) to B 4 Product of vector lengthdrawn from thezeroof GH ( ) ( ) to B Note : If zero doe not exit in tranfer function then we conider unity length. Hence, the correct option i (B). 5

26 Quetion 47 [Practice Book] [IES EC 11] Loop tranfer function of unity feedback ytem i the ytem i j G () ( 64) ( 16). The correct root locu diagram for j (A) (B) j j (C) (D) An. (D) Sol. ( 64) Given : G () ( 16) Number of pole, P =, Number of zero, Z = Total branche of root locu = Number of aymptote = P Z = 1 Angle of aymptote 18 The ytem ha pole at j4 and at and zero at j8. Pole zero location are hown in figure below, Angle of departure at pole at j4 j j8 d1 18 j4 Where, z p p p p z z 1z j4 j8 d1 18 ( 18 ) d at pole at 4 d j 6

27 Hence, the root locu i hown below, in which branche of root locu are tarting from pole and are terminating on zero, one pole will be terminating at zero preent in infinite -plane following the aymptote of 18. j 18 7

Chapter 7. Root Locus Analysis

Chapter 7. Root Locus Analysis Chapter 7 Root Locu Analyi jw + KGH ( ) GH ( ) - K 0 z O 4 p 2 p 3 p Root Locu Analyi The root of the cloed-loop characteritic equation define the ytem characteritic repone. Their location in the complex

More information

Root Locus Diagram. Root loci: The portion of root locus when k assume positive values: that is 0

Root Locus Diagram. Root loci: The portion of root locus when k assume positive values: that is 0 Objective Root Locu Diagram Upon completion of thi chapter you will be able to: Plot the Root Locu for a given Tranfer Function by varying gain of the ytem, Analye the tability of the ytem from the root

More information

ME2142/ME2142E Feedback Control Systems

ME2142/ME2142E Feedback Control Systems Root Locu Analyi Root Locu Analyi Conider the cloed-loop ytem R + E - G C B H The tranient repone, and tability, of the cloed-loop ytem i determined by the value of the root of the characteritic equation

More information

MODERN CONTROL SYSTEMS

MODERN CONTROL SYSTEMS MODERN CONTROL SYSTEMS Lecture 1 Root Locu Emam Fathy Department of Electrical and Control Engineering email: emfmz@aat.edu http://www.aat.edu/cv.php?dip_unit=346&er=68525 1 Introduction What i root locu?

More information

Automatic Control Systems. Part III: Root Locus Technique

Automatic Control Systems. Part III: Root Locus Technique www.pdhcenter.com PDH Coure E40 www.pdhonline.org Automatic Control Sytem Part III: Root Locu Technique By Shih-Min Hu, Ph.D., P.E. Page of 30 www.pdhcenter.com PDH Coure E40 www.pdhonline.org VI. Root

More information

Lecture 12: Examples of Root Locus Plots. Dr. Kalyana Veluvolu. Lecture 12: Examples of Root Locus Plots Dr. Kalyana Veluvolu

Lecture 12: Examples of Root Locus Plots. Dr. Kalyana Veluvolu. Lecture 12: Examples of Root Locus Plots Dr. Kalyana Veluvolu ROOT-LOCUS ANALYSIS Example: Given that G( ) ( + )( + ) Dr. alyana Veluvolu Sketch the root locu of 1 + G() and compute the value of that will yield a dominant econd order behavior with a damping ratio,

More information

Delhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubaneswar Kolkata Patna Web: Ph:

Delhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubaneswar Kolkata Patna Web:     Ph: Serial :. PT_EE_A+C_Control Sytem_798 Delhi Noida Bhopal Hyderabad Jaipur Lucknow Indore Pune Bhubanewar olkata Patna Web: E-mail: info@madeeay.in Ph: -4546 CLASS TEST 8-9 ELECTRICAL ENGINEERING Subject

More information

CISE302: Linear Control Systems

CISE302: Linear Control Systems Term 8 CISE: Linear Control Sytem Dr. Samir Al-Amer Chapter 7: Root locu CISE_ch 7 Al-Amer8 ١ Learning Objective Undertand the concept of root locu and it role in control ytem deign Be able to ketch root

More information

Figure 1: Unity Feedback System

Figure 1: Unity Feedback System MEM 355 Sample Midterm Problem Stability 1 a) I the following ytem table? Solution: G() = Pole: -1, -2, -2, -1.5000 + 1.3229i, -1.5000-1.3229i 1 ( + 1)( 2 + 3 + 4)( + 2) 2 A you can ee, all pole are on

More information

Root Locus Contents. Root locus, sketching algorithm. Root locus, examples. Root locus, proofs. Root locus, control examples

Root Locus Contents. Root locus, sketching algorithm. Root locus, examples. Root locus, proofs. Root locus, control examples Root Locu Content Root locu, ketching algorithm Root locu, example Root locu, proof Root locu, control example Root locu, influence of zero and pole Root locu, lead lag controller deign 9 Spring ME45 -

More information

ME 375 FINAL EXAM SOLUTIONS Friday December 17, 2004

ME 375 FINAL EXAM SOLUTIONS Friday December 17, 2004 ME 375 FINAL EXAM SOLUTIONS Friday December 7, 004 Diviion Adam 0:30 / Yao :30 (circle one) Name Intruction () Thi i a cloed book eamination, but you are allowed three 8.5 crib heet. () You have two hour

More information

Control Systems Analysis and Design by the Root-Locus Method

Control Systems Analysis and Design by the Root-Locus Method 6 Control Sytem Analyi and Deign by the Root-Locu Method 6 1 INTRODUCTION The baic characteritic of the tranient repone of a cloed-loop ytem i cloely related to the location of the cloed-loop pole. If

More information

ROOT LOCUS. Poles and Zeros

ROOT LOCUS. Poles and Zeros Automatic Control Sytem, 343 Deartment of Mechatronic Engineering, German Jordanian Univerity ROOT LOCUS The Root Locu i the ath of the root of the characteritic equation traced out in the - lane a a ytem

More information

Feedback Control Systems (FCS)

Feedback Control Systems (FCS) Feedback Control Sytem (FCS) Lecture19-20 Routh-Herwitz Stability Criterion Dr. Imtiaz Huain email: imtiaz.huain@faculty.muet.edu.pk URL :http://imtiazhuainkalwar.weebly.com/ Stability of Higher Order

More information

EE Control Systems LECTURE 14

EE Control Systems LECTURE 14 Updated: Tueday, March 3, 999 EE 434 - Control Sytem LECTURE 4 Copyright FL Lewi 999 All right reerved ROOT LOCUS DESIGN TECHNIQUE Suppoe the cloed-loop tranfer function depend on a deign parameter k We

More information

MEM 355 Performance Enhancement of Dynamical Systems Root Locus Analysis

MEM 355 Performance Enhancement of Dynamical Systems Root Locus Analysis MEM 355 Performance Enhancement of Dynamical Sytem Root Locu Analyi Harry G. Kwatny Department of Mechanical Engineering & Mechanic Drexel Univerity Outline The root locu method wa introduced by Evan in

More information

The state variable description of an LTI system is given by 3 1O. Statement for Linked Answer Questions 3 and 4 :

The state variable description of an LTI system is given by 3 1O. Statement for Linked Answer Questions 3 and 4 : CHAPTER 6 CONTROL SYSTEMS YEAR TO MARKS MCQ 6. The tate variable decription of an LTI ytem i given by Jxo N J a NJx N JN K O K OK O K O xo a x + u Kxo O K 3 a3 OKx O K 3 O L P L J PL P L P x N K O y _

More information

The Root Locus Method

The Root Locus Method The Root Locu Method MEM 355 Performance Enhancement of Dynamical Sytem Harry G. Kwatny Department of Mechanical Engineering & Mechanic Drexel Univerity Outline The root locu method wa introduced by Evan

More information

Chapter 13. Root Locus Introduction

Chapter 13. Root Locus Introduction Chapter 13 Root Locu 13.1 Introduction In the previou chapter we had a glimpe of controller deign iue through ome imple example. Obviouly when we have higher order ytem, uch imple deign technique will

More information

Chapter #4 EEE Automatic Control

Chapter #4 EEE Automatic Control Spring 008 EEE 00 Chapter #4 EEE 00 Automatic Control Root Locu Chapter 4 /4 Spring 008 EEE 00 Introduction Repone depend on ytem and controller parameter > Cloed loop pole location depend on ytem and

More information

Stability Criterion Routh Hurwitz

Stability Criterion Routh Hurwitz EES404 Fundamental of Control Sytem Stability Criterion Routh Hurwitz DR. Ir. Wahidin Wahab M.Sc. Ir. Arie Subiantoro M.Sc. Stability A ytem i table if for a finite input the output i imilarly finite A

More information

Function and Impulse Response

Function and Impulse Response Tranfer Function and Impule Repone Solution of Selected Unolved Example. Tranfer Function Q.8 Solution : The -domain network i hown in the Fig... Applying VL to the two loop, R R R I () I () L I () L V()

More information

Control Systems. Root locus.

Control Systems. Root locus. Control Sytem Root locu chibum@eoultech.ac.kr Outline Concet of Root Locu Contructing root locu Control Sytem Root Locu Stability and tranient reone i cloely related with the location of ole in -lane How

More information

March 18, 2014 Academic Year 2013/14

March 18, 2014 Academic Year 2013/14 POLITONG - SHANGHAI BASIC AUTOMATIC CONTROL Exam grade March 8, 4 Academic Year 3/4 NAME (Pinyin/Italian)... STUDENT ID Ue only thee page (including the back) for anwer. Do not ue additional heet. Ue of

More information

Control Systems. Root locus.

Control Systems. Root locus. Control Sytem Root locu chibum@eoultech.ac.kr Outline Concet of Root Locu Contructing root locu Control Sytem Root Locu Stability and tranient reone i cloely related with the location of ole in -lane How

More information

Linear System Fundamentals

Linear System Fundamentals Linear Sytem Fundamental MEM 355 Performance Enhancement of Dynamical Sytem Harry G. Kwatny Department of Mechanical Engineering & Mechanic Drexel Univerity Content Sytem Repreentation Stability Concept

More information

G(s) = 1 s by hand for! = 1, 2, 5, 10, 20, 50, and 100 rad/sec.

G(s) = 1 s by hand for! = 1, 2, 5, 10, 20, 50, and 100 rad/sec. 6003 where A = jg(j!)j ; = tan Im [G(j!)] Re [G(j!)] = \G(j!) 2. (a) Calculate the magnitude and phae of G() = + 0 by hand for! =, 2, 5, 0, 20, 50, and 00 rad/ec. (b) ketch the aymptote for G() according

More information

7.4 STEP BY STEP PROCEDURE TO DRAW THE ROOT LOCUS DIAGRAM

7.4 STEP BY STEP PROCEDURE TO DRAW THE ROOT LOCUS DIAGRAM ROOT LOCUS TECHNIQUE. Values of on the root loci The value of at any point s on the root loci is determined from the following equation G( s) H( s) Product of lengths of vectors from poles of G( s)h( s)

More information

Figure 1 Siemens PSSE Web Site

Figure 1 Siemens PSSE Web Site Stability Analyi of Dynamic Sytem. In the lat few lecture we have een how mall ignal Lalace domain model may be contructed of the dynamic erformance of ower ytem. The tability of uch ytem i a matter of

More information

ME 375 FINAL EXAM Wednesday, May 6, 2009

ME 375 FINAL EXAM Wednesday, May 6, 2009 ME 375 FINAL EXAM Wedneday, May 6, 9 Diviion Meckl :3 / Adam :3 (circle one) Name_ Intruction () Thi i a cloed book examination, but you are allowed three ingle-ided 8.5 crib heet. A calculator i NOT allowed.

More information

NAME (pinyin/italian)... MATRICULATION NUMBER... SIGNATURE

NAME (pinyin/italian)... MATRICULATION NUMBER... SIGNATURE POLITONG SHANGHAI BASIC AUTOMATIC CONTROL June Academic Year / Exam grade NAME (pinyin/italian)... MATRICULATION NUMBER... SIGNATURE Ue only thee page (including the bac) for anwer. Do not ue additional

More information

ECE 345 / ME 380 Introduction to Control Systems Lecture Notes 8

ECE 345 / ME 380 Introduction to Control Systems Lecture Notes 8 Learning Objectives ECE 345 / ME 380 Introduction to Control Systems Lecture Notes 8 Dr. Oishi oishi@unm.edu November 2, 203 State the phase and gain properties of a root locus Sketch a root locus, by

More information

CHAPTER # 9 ROOT LOCUS ANALYSES

CHAPTER # 9 ROOT LOCUS ANALYSES F K א CHAPTER # 9 ROOT LOCUS ANALYSES 1. Introduction The basic characteristic of the transient response of a closed-loop system is closely related to the location of the closed-loop poles. If the system

More information

Stability. ME 344/144L Prof. R.G. Longoria Dynamic Systems and Controls/Lab. Department of Mechanical Engineering The University of Texas at Austin

Stability. ME 344/144L Prof. R.G. Longoria Dynamic Systems and Controls/Lab. Department of Mechanical Engineering The University of Texas at Austin Stability The tability of a ytem refer to it ability or tendency to eek a condition of tatic equilibrium after it ha been diturbed. If given a mall perturbation from the equilibrium, it i table if it return.

More information

CONTROL SYSTEMS. Chapter 2 : Block Diagram & Signal Flow Graphs GATE Objective & Numerical Type Questions

CONTROL SYSTEMS. Chapter 2 : Block Diagram & Signal Flow Graphs GATE Objective & Numerical Type Questions ONTOL SYSTEMS hapter : Bloc Diagram & Signal Flow Graph GATE Objective & Numerical Type Quetion Quetion 6 [Practice Boo] [GATE E 994 IIT-Kharagpur : 5 Mar] educe the ignal flow graph hown in figure below,

More information

Analysis of Stability &

Analysis of Stability & INC 34 Feedback Control Sytem Analyi of Stability & Steady-State Error S Wonga arawan.won@kmutt.ac.th Summary from previou cla Firt-order & econd order ytem repone τ ωn ζω ω n n.8.6.4. ζ ζ. ζ.5 ζ ζ.5 ct.8.6.4...4.6.8..4.6.8

More information

Digital Control System

Digital Control System Digital Control Sytem - A D D A Micro ADC DAC Proceor Correction Element Proce Clock Meaurement A: Analog D: Digital Continuou Controller and Digital Control Rt - c Plant yt Continuou Controller Digital

More information

Lecture 10 Filtering: Applied Concepts

Lecture 10 Filtering: Applied Concepts Lecture Filtering: Applied Concept In the previou two lecture, you have learned about finite-impule-repone (FIR) and infinite-impule-repone (IIR) filter. In thee lecture, we introduced the concept of filtering

More information

Department of Mechanical Engineering Massachusetts Institute of Technology Modeling, Dynamics and Control III Spring 2002

Department of Mechanical Engineering Massachusetts Institute of Technology Modeling, Dynamics and Control III Spring 2002 Department of Mechanical Engineering Maachuett Intitute of Technology 2.010 Modeling, Dynamic and Control III Spring 2002 SOLUTIONS: Problem Set # 10 Problem 1 Etimating tranfer function from Bode Plot.

More information

Lecture 1 Root Locus

Lecture 1 Root Locus Root Locus ELEC304-Alper Erdogan 1 1 Lecture 1 Root Locus What is Root-Locus? : A graphical representation of closed loop poles as a system parameter varied. Based on Root-Locus graph we can choose the

More information

Solutions. Digital Control Systems ( ) 120 minutes examination time + 15 minutes reading time at the beginning of the exam

Solutions. Digital Control Systems ( ) 120 minutes examination time + 15 minutes reading time at the beginning of the exam BSc - Sample Examination Digital Control Sytem (5-588-) Prof. L. Guzzella Solution Exam Duration: Number of Quetion: Rating: Permitted aid: minute examination time + 5 minute reading time at the beginning

More information

Automatic Control Systems, 9th Edition

Automatic Control Systems, 9th Edition Chapter 7: Root Locus Analysis Appendix E: Properties and Construction of the Root Loci Automatic Control Systems, 9th Edition Farid Golnaraghi, Simon Fraser University Benjamin C. Kuo, University of Illinois

More information

MAE140 Linear Circuits Fall 2012 Final, December 13th

MAE140 Linear Circuits Fall 2012 Final, December 13th MAE40 Linear Circuit Fall 202 Final, December 3th Intruction. Thi exam i open book. You may ue whatever written material you chooe, including your cla note and textbook. You may ue a hand calculator with

More information

Math 273 Solutions to Review Problems for Exam 1

Math 273 Solutions to Review Problems for Exam 1 Math 7 Solution to Review Problem for Exam True or Fale? Circle ONE anwer for each Hint: For effective tudy, explain why if true and give a counterexample if fale (a) T or F : If a b and b c, then a c

More information

CHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL

CHAPTER 4 DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL 98 CHAPTER DESIGN OF STATE FEEDBACK CONTROLLERS AND STATE OBSERVERS USING REDUCED ORDER MODEL INTRODUCTION The deign of ytem uing tate pace model for the deign i called a modern control deign and it i

More information

Control Systems Engineering ( Chapter 8. Root Locus Techniques ) Prof. Kwang-Chun Ho Tel: Fax:

Control Systems Engineering ( Chapter 8. Root Locus Techniques ) Prof. Kwang-Chun Ho Tel: Fax: Control Systems Engineering ( Chapter 8. Root Locus Techniques ) Prof. Kwang-Chun Ho kwangho@hansung.ac.kr Tel: 02-760-4253 Fax:02-760-4435 Introduction In this lesson, you will learn the following : The

More information

Root locus Analysis. P.S. Gandhi Mechanical Engineering IIT Bombay. Acknowledgements: Mr Chaitanya, SYSCON 07

Root locus Analysis. P.S. Gandhi Mechanical Engineering IIT Bombay. Acknowledgements: Mr Chaitanya, SYSCON 07 Root locus Analysis P.S. Gandhi Mechanical Engineering IIT Bombay Acknowledgements: Mr Chaitanya, SYSCON 07 Recap R(t) + _ k p + k s d 1 s( s+ a) C(t) For the above system the closed loop transfer function

More information

EE Control Systems LECTURE 6

EE Control Systems LECTURE 6 Copyright FL Lewi 999 All right reerved EE - Control Sytem LECTURE 6 Updated: Sunday, February, 999 BLOCK DIAGRAM AND MASON'S FORMULA A linear time-invariant (LTI) ytem can be repreented in many way, including:

More information

ECE-320 Linear Control Systems. Spring 2014, Exam 1. No calculators or computers allowed, you may leave your answers as fractions.

ECE-320 Linear Control Systems. Spring 2014, Exam 1. No calculators or computers allowed, you may leave your answers as fractions. ECE-0 Linear Control Sytem Spring 04, Exam No calculator or computer allowed, you may leave your anwer a fraction. All problem are worth point unle noted otherwie. Total /00 Problem - refer to the unit

More information

Bogoliubov Transformation in Classical Mechanics

Bogoliubov Transformation in Classical Mechanics Bogoliubov Tranformation in Claical Mechanic Canonical Tranformation Suppoe we have a et of complex canonical variable, {a j }, and would like to conider another et of variable, {b }, b b ({a j }). How

More information

Advanced D-Partitioning Analysis and its Comparison with the Kharitonov s Theorem Assessment

Advanced D-Partitioning Analysis and its Comparison with the Kharitonov s Theorem Assessment Journal of Multidiciplinary Engineering Science and Technology (JMEST) ISSN: 59- Vol. Iue, January - 5 Advanced D-Partitioning Analyi and it Comparion with the haritonov Theorem Aement amen M. Yanev Profeor,

More information

Chapter 8. Root Locus Techniques

Chapter 8. Root Locus Techniques Chapter 8 Rt Lcu Technique Intrductin Sytem perfrmance and tability dt determined dby cled-lp l ple Typical cled-lp feedback cntrl ytem G Open-lp TF KG H Zer -, - Ple 0, -, -4 K 4 Lcatin f ple eaily fund

More information

Control Systems Engineering ( Chapter 7. Steady-State Errors ) Prof. Kwang-Chun Ho Tel: Fax:

Control Systems Engineering ( Chapter 7. Steady-State Errors ) Prof. Kwang-Chun Ho Tel: Fax: Control Sytem Engineering ( Chapter 7. Steady-State Error Prof. Kwang-Chun Ho kwangho@hanung.ac.kr Tel: 0-760-453 Fax:0-760-4435 Introduction In thi leon, you will learn the following : How to find the

More information

Lecture 21. The Lovasz splitting-off lemma Topics in Combinatorial Optimization April 29th, 2004

Lecture 21. The Lovasz splitting-off lemma Topics in Combinatorial Optimization April 29th, 2004 18.997 Topic in Combinatorial Optimization April 29th, 2004 Lecture 21 Lecturer: Michel X. Goeman Scribe: Mohammad Mahdian 1 The Lovaz plitting-off lemma Lovaz plitting-off lemma tate the following. Theorem

More information

Chapter 7 : Root Locus Technique

Chapter 7 : Root Locus Technique Chapter 7 : Root Locus Technique By Electrical Engineering Department College of Engineering King Saud University 1431-143 7.1. Introduction 7.. Basics on the Root Loci 7.3. Characteristics of the Loci

More information

LINEAR CONTROL SYSTEMS

LINEAR CONTROL SYSTEMS LINEAR CONTROL SYSTEMS Ali Karimpour Aociate Profeor Ferdowi Univerity of Mahhad Root Locu Criteria Topic to be covered include: v v v v Root locu criterion. u u u Root loci (RL). Complement root loci

More information

Lecture 7 CONTROL ENGINEERING. Ali Karimpour Associate Professor Ferdowsi University of Mashhad

Lecture 7 CONTROL ENGINEERING. Ali Karimpour Associate Professor Ferdowsi University of Mashhad CONTROL ENGINEERING Ali Karimpour Aociate Profeor Ferdowi Univerity of Mahhad Dr. Ali Karimpour Sep 5 Root Locu Criteria Topic to be covered include: Root locu criterion. Root loci (RL). Complement root

More information

SKEE 3143 CONTROL SYSTEM DESIGN. CHAPTER 3 Compensator Design Using the Bode Plot

SKEE 3143 CONTROL SYSTEM DESIGN. CHAPTER 3 Compensator Design Using the Bode Plot SKEE 3143 CONTROL SYSTEM DESIGN CHAPTER 3 Compenator Deign Uing the Bode Plot 1 Chapter Outline 3.1 Introduc4on Re- viit to Frequency Repone, ploang frequency repone, bode plot tability analyi. 3.2 Gain

More information

Given the following circuit with unknown initial capacitor voltage v(0): X(s) Immediately, we know that the transfer function H(s) is

Given the following circuit with unknown initial capacitor voltage v(0): X(s) Immediately, we know that the transfer function H(s) is EE 4G Note: Chapter 6 Intructor: Cheung More about ZSR and ZIR. Finding unknown initial condition: Given the following circuit with unknown initial capacitor voltage v0: F v0/ / Input xt 0Ω Output yt -

More information

SECTION 5: ROOT LOCUS ANALYSIS

SECTION 5: ROOT LOCUS ANALYSIS SECTION 5: ROOT LOCUS ANALYSIS MAE 4421 Control of Aerospace & Mechanical Systems 2 Introduction Introduction 3 Consider a general feedback system: Closed loop transfer function is 1 is the forward path

More information

1 Routh Array: 15 points

1 Routh Array: 15 points EE C28 / ME34 Problem Set 3 Solution Fall 2 Routh Array: 5 point Conider the ytem below, with D() k(+), w(t), G() +2, and H y() 2 ++2 2(+). Find the cloed loop tranfer function Y () R(), and range of k

More information

376 CHAPTER 6. THE FREQUENCY-RESPONSE DESIGN METHOD. D(s) = we get the compensated system with :

376 CHAPTER 6. THE FREQUENCY-RESPONSE DESIGN METHOD. D(s) = we get the compensated system with : 376 CHAPTER 6. THE FREQUENCY-RESPONSE DESIGN METHOD Therefore by applying the lead compenator with ome gain adjutment : D() =.12 4.5 +1 9 +1 we get the compenated ytem with : PM =65, ω c = 22 rad/ec, o

More information

Mathematical modeling of control systems. Laith Batarseh. Mathematical modeling of control systems

Mathematical modeling of control systems. Laith Batarseh. Mathematical modeling of control systems Chapter two Laith Batareh Mathematical modeling The dynamic of many ytem, whether they are mechanical, electrical, thermal, economic, biological, and o on, may be decribed in term of differential equation

More information

a. Closed-loop system; b. equivalent transfer function Then the CLTF () T is s the poles of () T are s from a contribution of a

a. Closed-loop system; b. equivalent transfer function Then the CLTF () T is s the poles of () T are s from a contribution of a Root Locus Simple definition Locus of points on the s- plane that represents the poles of a system as one or more parameter vary. RL and its relation to poles of a closed loop system RL and its relation

More information

Root locus 5. tw4 = 450. Root Locus S5-1 S O L U T I O N S

Root locus 5. tw4 = 450. Root Locus S5-1 S O L U T I O N S Root Locus S5-1 S O L U T I O N S Root locus 5 Note: All references to Figures and Equations whose numbers are not preceded by an "S" refer to the textbook. (a) Rule 2 is all that is required to find the

More information

Laplace Transformation

Laplace Transformation Univerity of Technology Electromechanical Department Energy Branch Advance Mathematic Laplace Tranformation nd Cla Lecture 6 Page of 7 Laplace Tranformation Definition Suppoe that f(t) i a piecewie continuou

More information

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS 8.1 INTRODUCTION 8.2 REDUCED ORDER MODEL DESIGN FOR LINEAR DISCRETE-TIME CONTROL SYSTEMS 8.3

More information

Massachusetts Institute of Technology Dynamics and Control II

Massachusetts Institute of Technology Dynamics and Control II I E Maachuett Intitute of Technology Department of Mechanical Engineering 2.004 Dynamic and Control II Laboratory Seion 5: Elimination of Steady-State Error Uing Integral Control Action 1 Laboratory Objective:

More information

Question 1 Equivalent Circuits

Question 1 Equivalent Circuits MAE 40 inear ircuit Fall 2007 Final Intruction ) Thi exam i open book You may ue whatever written material you chooe, including your cla note and textbook You may ue a hand calculator with no communication

More information

Course roadmap. ME451: Control Systems. What is Root Locus? (Review) Characteristic equation & root locus. Lecture 18 Root locus: Sketch of proofs

Course roadmap. ME451: Control Systems. What is Root Locus? (Review) Characteristic equation & root locus. Lecture 18 Root locus: Sketch of proofs ME451: Control Systems Modeling Course roadmap Analysis Design Lecture 18 Root locus: Sketch of proofs Dr. Jongeun Choi Department of Mechanical Engineering Michigan State University Laplace transform

More information

Riemann s Functional Equation is Not Valid and its Implication on the Riemann Hypothesis. Armando M. Evangelista Jr.

Riemann s Functional Equation is Not Valid and its Implication on the Riemann Hypothesis. Armando M. Evangelista Jr. Riemann Functional Equation i Not Valid and it Implication on the Riemann Hypothei By Armando M. Evangelita Jr. On November 4, 28 ABSTRACT Riemann functional equation wa formulated by Riemann that uppoedly

More information

Digital Control System

Digital Control System Digital Control Sytem Summary # he -tranform play an important role in digital control and dicrete ignal proceing. he -tranform i defined a F () f(k) k () A. Example Conider the following equence: f(k)

More information

Riemann s Functional Equation is Not a Valid Function and Its Implication on the Riemann Hypothesis. Armando M. Evangelista Jr.

Riemann s Functional Equation is Not a Valid Function and Its Implication on the Riemann Hypothesis. Armando M. Evangelista Jr. Riemann Functional Equation i Not a Valid Function and It Implication on the Riemann Hypothei By Armando M. Evangelita Jr. armando78973@gmail.com On Augut 28, 28 ABSTRACT Riemann functional equation wa

More information

EE/ME/AE324: Dynamical Systems. Chapter 8: Transfer Function Analysis

EE/ME/AE324: Dynamical Systems. Chapter 8: Transfer Function Analysis EE/ME/AE34: Dynamical Sytem Chapter 8: Tranfer Function Analyi The Sytem Tranfer Function Conider the ytem decribed by the nth-order I/O eqn.: ( n) ( n 1) ( m) y + a y + + a y = b u + + bu n 1 0 m 0 Taking

More information

6.447 rad/sec and ln (% OS /100) tan Thus pc. the testing point is s 3.33 j5.519

6.447 rad/sec and ln (% OS /100) tan Thus pc. the testing point is s 3.33 j5.519 9. a. 3.33, n T ln(% OS /100) 2 2 ln (% OS /100) 0.517. Thu n 6.7 rad/ec and the teting point i 3.33 j5.519. b. Summation of angle including the compenating zero i -106.691, The compenator pole mut contribute

More information

ECE 3510 Root Locus Design Examples. PI To eliminate steady-state error (for constant inputs) & perfect rejection of constant disturbances

ECE 3510 Root Locus Design Examples. PI To eliminate steady-state error (for constant inputs) & perfect rejection of constant disturbances ECE 350 Root Locu Deign Example Recall the imple crude ervo from lab G( ) 0 6.64 53.78 σ = = 3 23.473 PI To eliminate teady-tate error (for contant input) & perfect reection of contant diturbance Note:

More information

Linear Motion, Speed & Velocity

Linear Motion, Speed & Velocity Add Important Linear Motion, Speed & Velocity Page: 136 Linear Motion, Speed & Velocity NGSS Standard: N/A MA Curriculum Framework (006): 1.1, 1. AP Phyic 1 Learning Objective: 3.A.1.1, 3.A.1.3 Knowledge/Undertanding

More information

FRTN10 Exercise 3. Specifications and Disturbance Models

FRTN10 Exercise 3. Specifications and Disturbance Models FRTN0 Exercie 3. Specification and Diturbance Model 3. A feedback ytem i hown in Figure 3., in which a firt-order proce if controlled by an I controller. d v r u 2 z C() P() y n Figure 3. Sytem in Problem

More information

SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. Solutions to Assignment 3 February 2005.

SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. Solutions to Assignment 3 February 2005. SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuit II Solution to Aignment 3 February 2005. Initial Condition Source 0 V battery witch flip at t 0 find i 3 (t) Component value:

More information

Root Locus Methods. The root locus procedure

Root Locus Methods. The root locus procedure Root Locus Methods Design of a position control system using the root locus method Design of a phase lag compensator using the root locus method The root locus procedure To determine the value of the gain

More information

School of Mechanical Engineering Purdue University. DC Motor Position Control The block diagram for position control of the servo table is given by:

School of Mechanical Engineering Purdue University. DC Motor Position Control The block diagram for position control of the servo table is given by: Root Locus Motivation Sketching Root Locus Examples ME375 Root Locus - 1 Servo Table Example DC Motor Position Control The block diagram for position control of the servo table is given by: θ D 0.09 See

More information

"APPENDIX. Properties and Construction of the Root Loci " E-1 K ¼ 0ANDK ¼1POINTS

APPENDIX. Properties and Construction of the Root Loci  E-1 K ¼ 0ANDK ¼1POINTS Appendix-E_1 5/14/29 1 "APPENDIX E Properties and Construction of the Root Loci The following properties of the root loci are useful for constructing the root loci manually and for understanding the root

More information

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get Lecture 25 Introduction to Some Matlab c2d Code in Relation to Sampled Sytem here are many way to convert a continuou time function, { h( t) ; t [0, )} into a dicrete time function { h ( k) ; k {0,,, }}

More information

Chemical Process Dynamics and Control. Aisha Osman Mohamed Ahmed Department of Chemical Engineering Faculty of Engineering, Red Sea University

Chemical Process Dynamics and Control. Aisha Osman Mohamed Ahmed Department of Chemical Engineering Faculty of Engineering, Red Sea University Chemical Process Dynamics and Control Aisha Osman Mohamed Ahmed Department of Chemical Engineering Faculty of Engineering, Red Sea University 1 Chapter 4 System Stability 2 Chapter Objectives End of this

More information

An Interesting Property of Hyperbolic Paraboloids

An Interesting Property of Hyperbolic Paraboloids Page v w Conider the generic hyperbolic paraboloid defined by the equation. u = where a and b are aumed a b poitive. For our purpoe u, v and w are a permutation of x, y, and z. A typical graph of uch a

More information

SOLUTIONS TO ALGEBRAIC GEOMETRY AND ARITHMETIC CURVES BY QING LIU. I will collect my solutions to some of the exercises in this book in this document.

SOLUTIONS TO ALGEBRAIC GEOMETRY AND ARITHMETIC CURVES BY QING LIU. I will collect my solutions to some of the exercises in this book in this document. SOLUTIONS TO ALGEBRAIC GEOMETRY AND ARITHMETIC CURVES BY QING LIU CİHAN BAHRAN I will collect my olution to ome of the exercie in thi book in thi document. Section 2.1 1. Let A = k[[t ]] be the ring of

More information

MATEMATIK Datum: Tid: eftermiddag. A.Heintz Telefonvakt: Anders Martinsson Tel.:

MATEMATIK Datum: Tid: eftermiddag. A.Heintz Telefonvakt: Anders Martinsson Tel.: MATEMATIK Datum: 20-08-25 Tid: eftermiddag GU, Chalmer Hjälpmedel: inga A.Heintz Telefonvakt: Ander Martinon Tel.: 073-07926. Löningar till tenta i ODE och matematik modellering, MMG5, MVE6. Define what

More information

Convex Hulls of Curves Sam Burton

Convex Hulls of Curves Sam Burton Convex Hull of Curve Sam Burton 1 Introduction Thi paper will primarily be concerned with determining the face of convex hull of curve of the form C = {(t, t a, t b ) t [ 1, 1]}, a < b N in R 3. We hall

More information

ECE382/ME482 Spring 2004 Homework 4 Solution November 14,

ECE382/ME482 Spring 2004 Homework 4 Solution November 14, ECE382/ME482 Spring 2004 Homework 4 Solution November 14, 2005 1 Solution to HW4 AP4.3 Intead of a contant or tep reference input, we are given, in thi problem, a more complicated reference path, r(t)

More information

Problem Set 8 Solutions

Problem Set 8 Solutions Deign and Analyi of Algorithm April 29, 2015 Maachuett Intitute of Technology 6.046J/18.410J Prof. Erik Demaine, Srini Devada, and Nancy Lynch Problem Set 8 Solution Problem Set 8 Solution Thi problem

More information

Root Locus. Signals and Systems: 3C1 Control Systems Handout 3 Dr. David Corrigan Electronic and Electrical Engineering

Root Locus. Signals and Systems: 3C1 Control Systems Handout 3 Dr. David Corrigan Electronic and Electrical Engineering Root Locus Signals and Systems: 3C1 Control Systems Handout 3 Dr. David Corrigan Electronic and Electrical Engineering corrigad@tcd.ie Recall, the example of the PI controller car cruise control system.

More information

Software Engineering 3DX3. Slides 8: Root Locus Techniques

Software Engineering 3DX3. Slides 8: Root Locus Techniques Software Engineering 3DX3 Slides 8: Root Locus Techniques Dr. Ryan Leduc Department of Computing and Software McMaster University Material based on Control Systems Engineering by N. Nise. c 2006, 2007

More information

I What is root locus. I System analysis via root locus. I How to plot root locus. Root locus (RL) I Uses the poles and zeros of the OL TF

I What is root locus. I System analysis via root locus. I How to plot root locus. Root locus (RL) I Uses the poles and zeros of the OL TF EE C28 / ME C34 Feedback Control Systems Lecture Chapter 8 Root Locus Techniques Lecture abstract Alexandre Bayen Department of Electrical Engineering & Computer Science University of California Berkeley

More information

Physics 2212 G Quiz #2 Solutions Spring 2018

Physics 2212 G Quiz #2 Solutions Spring 2018 Phyic 2212 G Quiz #2 Solution Spring 2018 I. (16 point) A hollow inulating phere ha uniform volume charge denity ρ, inner radiu R, and outer radiu 3R. Find the magnitude of the electric field at a ditance

More information

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505)

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505) EE 4443/5329 LAB 3: Control of Indutrial Sytem Simulation and Hardware Control (PID Deign) The Inverted Pendulum (ECP Sytem-Model: 505) Compiled by: Nitin Swamy Email: nwamy@lakehore.uta.edu Email: okuljaca@lakehore.uta.edu

More information

Gain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays

Gain and Phase Margins Based Delay Dependent Stability Analysis of Two- Area LFC System with Communication Delays Gain and Phae Margin Baed Delay Dependent Stability Analyi of Two- Area LFC Sytem with Communication Delay Şahin Sönmez and Saffet Ayaun Department of Electrical Engineering, Niğde Ömer Halidemir Univerity,

More information

Module 3F2: Systems and Control EXAMPLES PAPER 2 ROOT-LOCUS. Solutions

Module 3F2: Systems and Control EXAMPLES PAPER 2 ROOT-LOCUS. Solutions Cambridge University Engineering Dept. Third Year Module 3F: Systems and Control EXAMPLES PAPER ROOT-LOCUS Solutions. (a) For the system L(s) = (s + a)(s + b) (a, b both real) show that the root-locus

More information

Chapter #4 EEE8013. Linear Controller Design and State Space Analysis. Design of control system in state space using Matlab

Chapter #4 EEE8013. Linear Controller Design and State Space Analysis. Design of control system in state space using Matlab EEE83 hapter #4 EEE83 Linear ontroller Deign and State Space nalyi Deign of control ytem in tate pace uing Matlab. ontrollabilty and Obervability.... State Feedback ontrol... 5 3. Linear Quadratic Regulator

More information

EE302 - Feedback Systems Spring Lecture KG(s)H(s) = KG(s)

EE302 - Feedback Systems Spring Lecture KG(s)H(s) = KG(s) EE3 - Feedback Systems Spring 19 Lecturer: Asst. Prof. M. Mert Ankarali Lecture 1.. 1.1 Root Locus In control theory, root locus analysis is a graphical analysis method for investigating the change of

More information

At the end of this lesson, the students should be able to understand:

At the end of this lesson, the students should be able to understand: Intructional Objective: At the end of thi leon, the tudent hould be able to undertand: Baic failure mechanim of riveted joint. Concept of deign of a riveted joint. 1. Strength of riveted joint: Strength

More information