Observability and Constructability

Size: px
Start display at page:

Download "Observability and Constructability"

Transcription

1 Capitolo. INTRODUCTION 5. Observability and Constructability Observability problem: compute the initial state x(t ) using the information associated to the input and output functions u(t) and y(t) of the given dynamic system in the time interval t [t,t ]. Definition. The initial state x(t ) of a dynamic system is compatible with the input and output functions u( ) and y( ) in the time interval [t,t ] if relation y(τ) = η(τ,t,x(t ),u( )) holds for τ [t,t ]. Let: E (t,t,u( ),y( )) denote the set of all the initial states x(t ) compatible with the input and output functions u( ) and y( )in the time interval [t,t ]. Constructability problem: compute the final state x(t ) using the information associated to the input and output functions u(t) and y(t) of the given dynamic system in the time interval t [t,t ]. Definition. A final state x(t ) of a dynamic system is compatible with the input and output functions u( ) and y( ) in the time interval [t,t ] if it exists an initial state x(t ) E (t,t,u( ),y( )) such x(t ) = ψ(t,t,x(t ),u( )). Let: E + (t,t,u( ),y( )) denote the set of all the final states x(t ) compatible with the input and output functions u( ) and y( )in the time interval [t,t ]. For time-invariant systems the two sets E and E + are function only of the amplitude t t of the time interval and therefore in this case one can set t = and use the following simplified notation: E (t,u( ),y( )), E + (t,u( ),y( ))

2 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5. Discrete-time linear systems Let us consider the following discrete-time linear system S = (A, B, C, D): { x(k +) = Ax(k)+Bu(k) Observability: y(k) = Cx(k)+Du(k) Definition. The initial state x() is called unobservable in k steps if it belongs to the set E (k) = E (k,, ), that is if it is compatible with the zero input and zero output functions, u(τ) = and y(τ) =, in the time interval τ [, k ]: = y(τ) = CA τ x(), for τ [, k ] that is if:. = y() y(). y(k ) = C CẠ. CA k } {{ } O (k) x() = O (k)x() where O (k) denotes the observability matrix in k steps. ThesetE (k)ofalltheinitialstatesx()whichareunobservable in k steps is a vectorial space which is equal to the kernel of matrix O (k): E (k) = ker[o (k)] TheunobservablesubspacesE (k)satisfythefollowingchainofinclusions (n is the dimension of the state space): E () E ()... E (n) = E (n+) =... ThesmallestunobservablesubspaceE (n)isobtained,atmost,innsteps.

3 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.3 The set E of all the initial states x() unobservable (that is unobservable in any number of steps) is a vectorial state space which is equal to the set E (n) of all the state space unobservable in n steps: E = E (n) = ker[o (n)] The subspace E is called unobservable subspace of the system and can be determined as follows: C E = ker O O = CẠ. CA n where O = O (n) denotes the observability matrix of the system. Definition. A system S is called observable (or completely observable) if the subspace E is equal to the zero state. Property. A system S is observable if and only if one of these relations holds: kero = {} rango O = n The initial state x() E (k,u( ),y( )) is compatible with the input and output functions u( ) and y( ) in the time interval [,k[ if the following relation is satisfied for τ [,k ]: that is if y(τ) = CA τ x()+ τ i= CA τ i Bu(i)+Du(τ) y l (τ) = CA τ x() where y l (τ) = y(τ) τ i= CAτ i Bu(i) Du(τ) is the free output evolution ofthesystem. Functiony l (τ)can be easilycomputed if theinputandoutputfunctionsu(τ)andy(τ)areknownforτ [,k ].

4 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.4 For time-invariant linear system the following relation holds: E (k,u( ),y( )) = E (k,,y l ( )) Note: the set E (k,u( ),y( )) depends only on the parameter k and the fee output evolution y l (τ). Property. ThesetE (k,u( ),y( ))isa linearvariety whichcanbeobtainedaddingaparticularsolutionx() E (k,,y l ( ))totheunobservable subspace E (k) = E (k,,) in k steps. Graphical representation: E (k,u( ),y( )) = x()+e (k) E (k,u( ),y( )) E (k) x() Setting k = n in the previous relation, one obtains the set E (u( ),y( )) of all the initial states x() which are compatible with the functions u( ) and y( ) in any number of steps: E (u( ),y( )) = x()+e This set contains only one element x() for each couple of functions u( ) and y( ) is and only if E =, that is if the system is completely observable. So, the following property holds. Property. Ifalinearsystemisobservable,thenitexistsonly one initial state x() compatible with any couple of input and output functions u(k) and y(k) in the time inteval k [, n].

5 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.5 Constructability: Istheproblemoffindingthefinalstatex(k)attimek compatiblewiththe input and output functions u(),...,u(k ) and y(),...,y(k ). If the system is observable in k steps, then the set E (k,u( ),y( )) contains only one element x() and therefore the final state x(k) is unique: x(k) = A k x()+ k i= A k i Bu(i) On the contrary, if the system is unobservable in k steps, then it is E (k,u( ),y( )) = x()+e (k), and therefore the set E + (k, u( ), y( )), of all the final states x(k) compatible with the input and output functions u( ) and y( ) has the following structure: E + (k, u( ), y( )) = x(k)+a k E (k) }{{} E + (k) The set E + (k, u( ), y( )) is obtained adding a particular solution x(k) to the subspace E + (k) of all the final states non constructable in k steps: E + (k) = A k E (k) A system is constructable in k steps if E + (k) = A k E (k) = {}, that is E (k) kera k A system is constructable if it exists a k such that E (k) kera k. It takes n steps, at most, for a discrete system to be constructable. So, the constructability condition can be expressed in the following way: E = kero kera n Note: from this last relation it follows that the observabilty implies the constructability, but not vice versa: Observability Constructability

6 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.6 Example. Let us consider the following discrete linear system: x(k +) = x(k)+ u(k) y(k) = [ ] x(k) Compute the set of all the initial states x = x() compatible with the free output evolution: y() =, y() =, y() =. The observability matrix of the system is: O =, deto = 4 Since O is not singular, the system is completely observable, and therefore if the system has a solution, then it has only one solution. The solution x can be determined as follows: that is: y() y() y() = x = C CA CA x = O x x = [O ] = = y() y() y() So, the only initial state compatible with the given free output evolution is x = [,, ]. Note: the free output evolution y(τ) is also determined for τ 3: y(τ) = CA τ x

7 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.7 Example. Let us consider the following discrete linear system: x(k +) = x(k)+ u(k) y(k) = [ ] x(k) Compute the set of all the initial states x = x() compatible with the free output evolution: y() =, y() =, y() = 4. The system is not completely observable: O = E = span The set of all the initial conditions compatible with the free output evolution y() =, y() =, y() = 4 can be determined computing a particular solution x p and adding the unobservable space E. The particular solution x p can be determined solving the following equation 4 = x p y = O x p A solution exists because the vector y belongs to the image of matrix O. y Im(O ) x p = So, the set of all the initial states x compatible with the free output evolution is the following: x = x p +E = +span

8 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.8 Example. Let us consider the following discrete linear system: x(k +) = x(k)+ u(k) y(k) = [ ] x(k) Compute the set of all the initial states x = x() compatible with the free output evolution:: y() =, y() =, y() =. The observability matrix of the system is: O = 4 Since the rank of matrix O is, the system is not completely observable. The set of all the initial states x = x() compatible with the free output evolution: y() =, y() =, y() = satisfies the following relation: y = y() y() y() O x 4 The vector y cannot be obtained as linear combination of the columns of matrix O, and therefore the given problem does not have solutions. There are no initial states x which are compatible with the given free output evolution. Property. The initial state x of minimum norm which minimizes the Euclidean norm y O x is obtained as follows: x = (O ) T N(N T O (O ) T N) N T y where matrix N is a base matrix of Im(O ): Im(N) = Im(O ) x The columns of matrix N are a set of linearly independent columns of matrix O.

9 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.9 Invariant continuous-time linear systems Let S = (A, B, C, D) be an invariant continuous-time linear system: { ẋ(t) = Ax(t)+Bu(t) y(t) = Cx(t)+Du(t) The observability and constructability properties of the continuous-time systems are very similar to those described for of the discrete-time system. Observability: Definition. An initial state x() is unobservable in the time interval [, t] if it is compatible with the zero input and output functions, u(τ) = and y(τ) =, for τ [, t]: = Ce Aτ x(), for τ [, t] The set E (t) of the initial states x() unobservable in [, t] is a vectorial subspace: E (t) = kero t where O t denotes the linear operator O t : X Y(t) which provides the free output evolution y(τ) Y(t) corresponding to the initial state x() X: O t : x() Ce Aτ x(), τ t Property. The unobservable subspace E = E (t) does not depend on the length of the time interval t > and it is equal to the kernel of the same observability matrix O defied for the discrete-time systems. E = ker[o ] So, for continuous-time systems, the computation of the initial state x() compatible with the input and output functions u( ) and y( ) does not depend on the length of he time interval [, t], provided it is not zero, but it depends only on the rank of the observability matrix O.

10 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5. Constructability: For continuous-time system the observability is equivalent to the constructability. In fact, in this case, the unobservable and the unconstructable subspaces E and E + are linked by the following relation: E + = e At E Since matrix e At is always invertible, for any matrix A, the two subspaces E + and E always have the same dimension. Moreover, it can be proved that they are equal: E + = E From this last relation it follows that for continuous-time systems the osservability implies and is implied by the constructability: Observability Constructability

11 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5. Duality Given a continuousordiscrete-time systems = (A,B,C,D), the system S D = (A T,C T,B T,D T ), is called the dual system of system S. No. of inputs of system S = No. of outputs of system S D No. of outputs of system S = No. of inputs of system S D Reachability and observability properties. The reachability and observability matrices R + D and O D of the dual system S D are linked to the reachability and observability matrices R + and O of system S as follows: R + D = [CT A T C T...(A T ) n C T ] = O D = B T B T A T. B T (A T ) n C CẠ. CA n T = (O ) T = [B AB...A n B] T = (R + ) T Property. For the systems S and S D the following properties hold: S reachable S D observable S observable S D reachable S controllable S D constructable S constructable S D controllable If two equivalent systems S and S are linked by the state space transformation x = Tx, then the corresponding dual system S D and S D are linked by the state space transformation x D = Px D where P = T T : S = (A, B, C) Duality T S = (T AT, T B, CT) Duality S D = (A T, C T, B T ) P S D = (TT A T T T, T T C T, B T T T )

12 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5. Osservability standard form Property. A linear system S = {A, B, C, D} (continuous or discrete) not completely observable can always be brought into observability standard form, that is, system S is algebraically equivalent the a transformed system S = {A, B, C, D} where the matrices A = P AP, B = P B, C = CP and D have the following structure: [ ] [ ] A, B A = B = A, A, B C = [ C ] D = D Let be ρ = n dime < n. The transformation matrix P which brings the system into the observability standard form has the following structure: ] P = [ R R, x = Px where R R ρ n is composed by ρ linearly independent rows of the observability matrix O, and R R (n ρ) n is a free matrix chosen such that the transformation matrix P is non singular. Proprerty. The subsystem of dimension ρ characterized by matrices A, and C is completely observable. The subsystem (A,, B, C ), is called observable subsystem and it represents the part of the original system which is observable. The subsystem (A,, B, ), characterized by matrices A,, B and C =, is called unobservable subsystem and it represents the part of the system which does not influence in any way the system output y. Also in this case the eigenvalues of matrix A are split in two sets: the eigenvalues of the observable part of the system (the eigenvalues of matrix A, ) and the eigenvalues of the unobservable part (the eigenvalues of of matrix A, ).

13 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.3 For the discrete case, let us divide the state vector x(k) in two parts: the observable part x and the unobservable part x : x = [ ] T, x x where dimx = ρ. The equations of the system are: x (k +) = A, x (k)+ B u(k) x (k +) = A, x (k)+ A, x (k)+ B u(k) y(k) = C x (k)+ Du(k) The corresponding block scheme is: D B x (k +) z I ρ x (k) C y(k) u(k) A, A, B x (k +) z I n ρ x (k) A, A similar decomposition holds also for continuous-time systems. Property. The transfer matrix H(z) [o H(s) ] of a linear system is equal to the transfer matrix of the observable part: H(z) [o H(s) ] is influenced only by the matrices (A,, B, C ) of the observable subsystem. Proof. The transfer matrix H(z) = C(zI A) B = C(zI A) B is: H(z) = [ C ][ ] [ ] zi A, B = A, zi A, B = [ C ][ ][ ] (zi A, ) B (zi A, ) = = C (zi A, ) B B

14 Capitolo 5. OBSERVABILITY AND CONSTRUCTABILITY 5.4 Example. Let us consider the following time-continuous linear system ẋ(t) = x(t)+ u(t) y(t) = [ ] x(t) Bring the system in the observability standard form. Sol. The observability matrix of the system is: O = deto = 3 3 Matrix O is singular. The system is not completely observable and therefore it is possible to compute the transformation matrix P which brings the system into the observability standard form: P = P = The transformed system has the following form: x(t)= x(t)+ y(t)= [ ] x(t) u(t) The unobservable part of the system is simply stable because it has an eigenvalues located in the origin: s =. The transfer matrix: G(s) = C o (si A o ) B o = [ ][ s s+ if a function only of the observable part of the system. ] [ ] = (s+) s +3

Reachability and Controllability

Reachability and Controllability Capitolo. INTRODUCTION 4. Reachability and Controllability Reachability. The reachability problem is to find the set of all the final states x(t ) reachable starting from a given initial state x(t ) :

More information

Equilibrium points: continuous-time systems

Equilibrium points: continuous-time systems Capitolo 0 INTRODUCTION 81 Equilibrium points: continuous-time systems Let us consider the following continuous-time linear system ẋ(t) Ax(t)+Bu(t) y(t) Cx(t)+Du(t) The equilibrium points x 0 of the system

More information

Linear System Theory

Linear System Theory Linear System Theory Wonhee Kim Chapter 6: Controllability & Observability Chapter 7: Minimal Realizations May 2, 217 1 / 31 Recap State space equation Linear Algebra Solutions of LTI and LTV system Stability

More information

ECE504: Lecture 9. D. Richard Brown III. Worcester Polytechnic Institute. 04-Nov-2008

ECE504: Lecture 9. D. Richard Brown III. Worcester Polytechnic Institute. 04-Nov-2008 ECE504: Lecture 9 D. Richard Brown III Worcester Polytechnic Institute 04-Nov-2008 Worcester Polytechnic Institute D. Richard Brown III 04-Nov-2008 1 / 38 Lecture 9 Major Topics ECE504: Lecture 9 We are

More information

Observability. It was the property in Lyapunov stability which allowed us to resolve that

Observability. It was the property in Lyapunov stability which allowed us to resolve that Observability We have seen observability twice already It was the property which permitted us to retrieve the initial state from the initial data {u(0),y(0),u(1),y(1),...,u(n 1),y(n 1)} It was the property

More information

Systems and Control Theory Lecture Notes. Laura Giarré

Systems and Control Theory Lecture Notes. Laura Giarré Systems and Control Theory Lecture Notes Laura Giarré L. Giarré 2017-2018 Lesson 5: State Space Systems State Dimension Infinite-Dimensional systems State-space model (nonlinear) LTI State Space model

More information

Controllability, Observability, Full State Feedback, Observer Based Control

Controllability, Observability, Full State Feedback, Observer Based Control Multivariable Control Lecture 4 Controllability, Observability, Full State Feedback, Observer Based Control John T. Wen September 13, 24 Ref: 3.2-3.4 of Text Controllability ẋ = Ax + Bu; x() = x. At time

More information

Observability and state estimation

Observability and state estimation EE263 Autumn 2015 S Boyd and S Lall Observability and state estimation state estimation discrete-time observability observability controllability duality observers for noiseless case continuous-time observability

More information

Analysis of Discrete-Time Systems

Analysis of Discrete-Time Systems TU Berlin Discrete-Time Control Systems 1 Analysis of Discrete-Time Systems Overview Stability Sensitivity and Robustness Controllability, Reachability, Observability, and Detectabiliy TU Berlin Discrete-Time

More information

Chapter 6 Controllability and Obervability

Chapter 6 Controllability and Obervability Chapter 6 Controllability and Obervability Controllability: whether or not the state-space equation can be controlled from input. Observability: whether or not the initial state can be observed from output.

More information

ECEN 605 LINEAR SYSTEMS. Lecture 8 Invariant Subspaces 1/26

ECEN 605 LINEAR SYSTEMS. Lecture 8 Invariant Subspaces 1/26 1/26 ECEN 605 LINEAR SYSTEMS Lecture 8 Invariant Subspaces Subspaces Let ẋ(t) = A x(t) + B u(t) y(t) = C x(t) (1a) (1b) denote a dynamic system where X, U and Y denote n, r and m dimensional vector spaces,

More information

Systems and Control Theory Lecture Notes. Laura Giarré

Systems and Control Theory Lecture Notes. Laura Giarré Systems and Control Theory Lecture Notes Laura Giarré L. Giarré 2018-2019 Lesson 14: Rechability Reachability (DT) Reachability theorem (DT) Reachability properties (DT) Reachability gramian (DT) Reachability

More information

Control Systems Design

Control Systems Design ELEC4410 Control Systems Design Lecture 14: Controllability Julio H. Braslavsky julio@ee.newcastle.edu.au School of Electrical Engineering and Computer Science Lecture 14: Controllability p.1/23 Outline

More information

Control Systems Design, SC4026. SC4026 Fall 2009, dr. A. Abate, DCSC, TU Delft

Control Systems Design, SC4026. SC4026 Fall 2009, dr. A. Abate, DCSC, TU Delft Control Systems Design, SC4026 SC4026 Fall 2009, dr. A. Abate, DCSC, TU Delft Lecture 4 Controllability (a.k.a. Reachability) vs Observability Algebraic Tests (Kalman rank condition & Hautus test) A few

More information

Analysis of Discrete-Time Systems

Analysis of Discrete-Time Systems TU Berlin Discrete-Time Control Systems TU Berlin Discrete-Time Control Systems 2 Stability Definitions We define stability first with respect to changes in the initial conditions Analysis of Discrete-Time

More information

Control Systems Design, SC4026. SC4026 Fall 2010, dr. A. Abate, DCSC, TU Delft

Control Systems Design, SC4026. SC4026 Fall 2010, dr. A. Abate, DCSC, TU Delft Control Systems Design, SC4026 SC4026 Fall 2010, dr. A. Abate, DCSC, TU Delft Lecture 4 Controllability (a.k.a. Reachability) and Observability Algebraic Tests (Kalman rank condition & Hautus test) A few

More information

Solution for Homework 5

Solution for Homework 5 Solution for Homework 5 ME243A/ECE23A Fall 27 Exercise 1 The computation of the reachable subspace in continuous time can be handled easily introducing the concepts of inner product, orthogonal complement

More information

Module 08 Observability and State Estimator Design of Dynamical LTI Systems

Module 08 Observability and State Estimator Design of Dynamical LTI Systems Module 08 Observability and State Estimator Design of Dynamical LTI Systems Ahmad F. Taha EE 5143: Linear Systems and Control Email: ahmad.taha@utsa.edu Webpage: http://engineering.utsa.edu/ataha November

More information

3 Gramians and Balanced Realizations

3 Gramians and Balanced Realizations 3 Gramians and Balanced Realizations In this lecture, we use an optimization approach to find suitable realizations for truncation and singular perturbation of G. It turns out that the recommended realizations

More information

Lecture 19 Observability and state estimation

Lecture 19 Observability and state estimation EE263 Autumn 2007-08 Stephen Boyd Lecture 19 Observability and state estimation state estimation discrete-time observability observability controllability duality observers for noiseless case continuous-time

More information

Model reduction for linear systems by balancing

Model reduction for linear systems by balancing Model reduction for linear systems by balancing Bart Besselink Jan C. Willems Center for Systems and Control Johann Bernoulli Institute for Mathematics and Computer Science University of Groningen, Groningen,

More information

Linear Algebra Review. Vectors

Linear Algebra Review. Vectors Linear Algebra Review 9/4/7 Linear Algebra Review By Tim K. Marks UCSD Borrows heavily from: Jana Kosecka http://cs.gmu.edu/~kosecka/cs682.html Virginia de Sa (UCSD) Cogsci 8F Linear Algebra review Vectors

More information

S09 MTH 371 Linear Algebra NEW PRACTICE QUIZ 4, SOLUTIONS Prof. G.Todorov February 15, 2009 Please, justify your answers.

S09 MTH 371 Linear Algebra NEW PRACTICE QUIZ 4, SOLUTIONS Prof. G.Todorov February 15, 2009 Please, justify your answers. S09 MTH 37 Linear Algebra NEW PRACTICE QUIZ 4, SOLUTIONS Prof. G.Todorov February, 009 Please, justify your answers. 3 0. Let A = 0 3. 7 Determine whether the column vectors of A are dependent or independent.

More information

M340L Final Exam Solutions May 13, 1995

M340L Final Exam Solutions May 13, 1995 M340L Final Exam Solutions May 13, 1995 Name: Problem 1: Find all solutions (if any) to the system of equations. Express your answer in vector parametric form. The matrix in other words, x 1 + 2x 3 + 3x

More information

Contents. Preface for the Instructor. Preface for the Student. xvii. Acknowledgments. 1 Vector Spaces 1 1.A R n and C n 2

Contents. Preface for the Instructor. Preface for the Student. xvii. Acknowledgments. 1 Vector Spaces 1 1.A R n and C n 2 Contents Preface for the Instructor xi Preface for the Student xv Acknowledgments xvii 1 Vector Spaces 1 1.A R n and C n 2 Complex Numbers 2 Lists 5 F n 6 Digression on Fields 10 Exercises 1.A 11 1.B Definition

More information

Lecture 4 and 5 Controllability and Observability: Kalman decompositions

Lecture 4 and 5 Controllability and Observability: Kalman decompositions 1 Lecture 4 and 5 Controllability and Observability: Kalman decompositions Spring 2013 - EE 194, Advanced Control (Prof. Khan) January 30 (Wed.) and Feb. 04 (Mon.), 2013 I. OBSERVABILITY OF DT LTI SYSTEMS

More information

Kalman Decomposition B 2. z = T 1 x, where C = ( C. z + u (7) T 1, and. where B = T, and

Kalman Decomposition B 2. z = T 1 x, where C = ( C. z + u (7) T 1, and. where B = T, and Kalman Decomposition Controllable / uncontrollable decomposition Suppose that the controllability matrix C R n n of a system has rank n 1

More information

State space transformations

State space transformations Capitolo 0. INTRODUCTION. State space transformations Let us consider the following linear time-invariant system: { ẋ(t) = A(t)+Bu(t) y(t) = C(t)+Du(t) () A state space transformation can be obtained using

More information

PRACTICE FINAL EXAM. why. If they are dependent, exhibit a linear dependence relation among them.

PRACTICE FINAL EXAM. why. If they are dependent, exhibit a linear dependence relation among them. Prof A Suciu MTH U37 LINEAR ALGEBRA Spring 2005 PRACTICE FINAL EXAM Are the following vectors independent or dependent? If they are independent, say why If they are dependent, exhibit a linear dependence

More information

Chapter 3 Transformations

Chapter 3 Transformations Chapter 3 Transformations An Introduction to Optimization Spring, 2014 Wei-Ta Chu 1 Linear Transformations A function is called a linear transformation if 1. for every and 2. for every If we fix the bases

More information

Balanced Truncation 1

Balanced Truncation 1 Massachusetts Institute of Technology Department of Electrical Engineering and Computer Science 6.242, Fall 2004: MODEL REDUCTION Balanced Truncation This lecture introduces balanced truncation for LTI

More information

Module 03 Linear Systems Theory: Necessary Background

Module 03 Linear Systems Theory: Necessary Background Module 03 Linear Systems Theory: Necessary Background Ahmad F. Taha EE 5243: Introduction to Cyber-Physical Systems Email: ahmad.taha@utsa.edu Webpage: http://engineering.utsa.edu/ taha/index.html September

More information

Discrete and continuous dynamic systems

Discrete and continuous dynamic systems Discrete and continuous dynamic systems Bounded input bounded output (BIBO) and asymptotic stability Continuous and discrete time linear time-invariant systems Katalin Hangos University of Pannonia Faculty

More information

Controllability. Chapter Reachable States. This chapter develops the fundamental results about controllability and pole assignment.

Controllability. Chapter Reachable States. This chapter develops the fundamental results about controllability and pole assignment. Chapter Controllability This chapter develops the fundamental results about controllability and pole assignment Reachable States We study the linear system ẋ = Ax + Bu, t, where x(t) R n and u(t) R m Thus

More information

CME 345: MODEL REDUCTION

CME 345: MODEL REDUCTION CME 345: MODEL REDUCTION Balanced Truncation Charbel Farhat & David Amsallem Stanford University cfarhat@stanford.edu These slides are based on the recommended textbook: A.C. Antoulas, Approximation of

More information

EE263: Introduction to Linear Dynamical Systems Review Session 6

EE263: Introduction to Linear Dynamical Systems Review Session 6 EE263: Introduction to Linear Dynamical Systems Review Session 6 Outline diagonalizability eigen decomposition theorem applications (modal forms, asymptotic growth rate) EE263 RS6 1 Diagonalizability consider

More information

Linear Algebra. Grinshpan

Linear Algebra. Grinshpan Linear Algebra Grinshpan Saturday class, 2/23/9 This lecture involves topics from Sections 3-34 Subspaces associated to a matrix Given an n m matrix A, we have three subspaces associated to it The column

More information

ME 234, Lyapunov and Riccati Problems. 1. This problem is to recall some facts and formulae you already know. e Aτ BB e A τ dτ

ME 234, Lyapunov and Riccati Problems. 1. This problem is to recall some facts and formulae you already know. e Aτ BB e A τ dτ ME 234, Lyapunov and Riccati Problems. This problem is to recall some facts and formulae you already know. (a) Let A and B be matrices of appropriate dimension. Show that (A, B) is controllable if and

More information

1. Find the solution of the following uncontrolled linear system. 2 α 1 1

1. Find the solution of the following uncontrolled linear system. 2 α 1 1 Appendix B Revision Problems 1. Find the solution of the following uncontrolled linear system 0 1 1 ẋ = x, x(0) =. 2 3 1 Class test, August 1998 2. Given the linear system described by 2 α 1 1 ẋ = x +

More information

1 Continuous-time Systems

1 Continuous-time Systems Observability Completely controllable systems can be restructured by means of state feedback to have many desirable properties. But what if the state is not available for feedback? What if only the output

More information

v = w if the same length and the same direction Given v, we have the negative v. We denote the length of v by v.

v = w if the same length and the same direction Given v, we have the negative v. We denote the length of v by v. Linear Algebra [1] 4.1 Vectors and Lines Definition scalar : magnitude vector : magnitude and direction Geometrically, a vector v can be represented by an arrow. We denote the length of v by v. zero vector

More information

Intro. Computer Control Systems: F8

Intro. Computer Control Systems: F8 Intro. Computer Control Systems: F8 Properties of state-space descriptions and feedback Dave Zachariah Dept. Information Technology, Div. Systems and Control 1 / 22 dave.zachariah@it.uu.se F7: Quiz! 2

More information

Linear Algebra Practice Final

Linear Algebra Practice Final . Let (a) First, Linear Algebra Practice Final Summer 3 3 A = 5 3 3 rref([a ) = 5 so if we let x 5 = t, then x 4 = t, x 3 =, x = t, and x = t, so that t t x = t = t t whence ker A = span(,,,, ) and a basis

More information

x 3y 2z = 6 1.2) 2x 4y 3z = 8 3x + 6y + 8z = 5 x + 3y 2z + 5t = 4 1.5) 2x + 8y z + 9t = 9 3x + 5y 12z + 17t = 7

x 3y 2z = 6 1.2) 2x 4y 3z = 8 3x + 6y + 8z = 5 x + 3y 2z + 5t = 4 1.5) 2x + 8y z + 9t = 9 3x + 5y 12z + 17t = 7 Linear Algebra and its Applications-Lab 1 1) Use Gaussian elimination to solve the following systems x 1 + x 2 2x 3 + 4x 4 = 5 1.1) 2x 1 + 2x 2 3x 3 + x 4 = 3 3x 1 + 3x 2 4x 3 2x 4 = 1 x + y + 2z = 4 1.4)

More information

Some solutions of the written exam of January 27th, 2014

Some solutions of the written exam of January 27th, 2014 TEORIA DEI SISTEMI Systems Theory) Prof. C. Manes, Prof. A. Germani Some solutions of the written exam of January 7th, 0 Problem. Consider a feedback control system with unit feedback gain, with the following

More information

EEE582 Homework Problems

EEE582 Homework Problems EEE582 Homework Problems HW. Write a state-space realization of the linearized model for the cruise control system around speeds v = 4 (Section.3, http://tsakalis.faculty.asu.edu/notes/models.pdf). Use

More information

1 Similarity transform 2. 2 Controllability The PBH test for controllability Observability The PBH test for observability...

1 Similarity transform 2. 2 Controllability The PBH test for controllability Observability The PBH test for observability... Contents 1 Similarity transform 2 2 Controllability 3 21 The PBH test for controllability 5 3 Observability 6 31 The PBH test for observability 7 4 Example ([1, pp121) 9 5 Subspace decomposition 11 51

More information

Lecture 2. Linear Systems

Lecture 2. Linear Systems Lecture 2. Linear Systems Ivan Papusha CDS270 2: Mathematical Methods in Control and System Engineering April 6, 2015 1 / 31 Logistics hw1 due this Wed, Apr 8 hw due every Wed in class, or my mailbox on

More information

Family Feud Review. Linear Algebra. October 22, 2013

Family Feud Review. Linear Algebra. October 22, 2013 Review Linear Algebra October 22, 2013 Question 1 Let A and B be matrices. If AB is a 4 7 matrix, then determine the dimensions of A and B if A has 19 columns. Answer 1 Answer A is a 4 19 matrix, while

More information

Education in Linear System Theory with the Geometric Approach Tools

Education in Linear System Theory with the Geometric Approach Tools Education in Linear System Theory with the Geometric Approach Tools Giovanni Marro DEIS, University of Bologna, Italy GAS Workshop - Sept 24, 2010 Politecnico di Milano G. Marro (University of Bologna)

More information

Linear Algebra Massoud Malek

Linear Algebra Massoud Malek CSUEB Linear Algebra Massoud Malek Inner Product and Normed Space In all that follows, the n n identity matrix is denoted by I n, the n n zero matrix by Z n, and the zero vector by θ n An inner product

More information

Systems and Control Theory Lecture Notes. Laura Giarré

Systems and Control Theory Lecture Notes. Laura Giarré Systems and Control Theory Lecture Notes Laura Giarré L. Giarré 2017-2018 Lesson 7: Response of LTI systems in the transform domain Laplace Transform Transform-domain response (CT) Transfer function Zeta

More information

ECE504: Lecture 10. D. Richard Brown III. Worcester Polytechnic Institute. 11-Nov-2008

ECE504: Lecture 10. D. Richard Brown III. Worcester Polytechnic Institute. 11-Nov-2008 ECE504: Lecture 10 D. Richard Brown III Worcester Polytechnic Institute 11-Nov-2008 Worcester Polytechnic Institute D. Richard Brown III 11-Nov-2008 1 / 25 Lecture 10 Major Topics We are finishing up Part

More information

Control engineering sample exam paper - Model answers

Control engineering sample exam paper - Model answers Question Control engineering sample exam paper - Model answers a) By a direct computation we obtain x() =, x(2) =, x(3) =, x(4) = = x(). This trajectory is sketched in Figure (left). Note that A 2 = I

More information

Supplementary Notes on Linear Algebra

Supplementary Notes on Linear Algebra Supplementary Notes on Linear Algebra Mariusz Wodzicki May 3, 2015 1 Vector spaces 1.1 Coordinatization of a vector space 1.1.1 Given a basis B = {b 1,..., b n } in a vector space V, any vector v V can

More information

Math 415 Exam I. Name: Student ID: Calculators, books and notes are not allowed!

Math 415 Exam I. Name: Student ID: Calculators, books and notes are not allowed! Math 415 Exam I Calculators, books and notes are not allowed! Name: Student ID: Score: Math 415 Exam I (20pts) 1. Let A be a square matrix satisfying A 2 = 2A. Find the determinant of A. Sol. From A 2

More information

MATH 304 Linear Algebra Lecture 10: Linear independence. Wronskian.

MATH 304 Linear Algebra Lecture 10: Linear independence. Wronskian. MATH 304 Linear Algebra Lecture 10: Linear independence. Wronskian. Spanning set Let S be a subset of a vector space V. Definition. The span of the set S is the smallest subspace W V that contains S. If

More information

Systems and Control Theory Lecture Notes. Laura Giarré

Systems and Control Theory Lecture Notes. Laura Giarré Systems and Control Theory Lecture Notes Laura Giarré L. Giarré 20182019 Lesson 14: Rechability I Reachability (DT) I Reachability theorem (DT) I Reachability properties (DT) I Reachability gramian (DT)

More information

1. What is the determinant of the following matrix? a 1 a 2 4a 3 2a 2 b 1 b 2 4b 3 2b c 1. = 4, then det

1. What is the determinant of the following matrix? a 1 a 2 4a 3 2a 2 b 1 b 2 4b 3 2b c 1. = 4, then det What is the determinant of the following matrix? 3 4 3 4 3 4 4 3 A 0 B 8 C 55 D 0 E 60 If det a a a 3 b b b 3 c c c 3 = 4, then det a a 4a 3 a b b 4b 3 b c c c 3 c = A 8 B 6 C 4 D E 3 Let A be an n n matrix

More information

Modelling and Control of Dynamic Systems. Stability of Linear Systems. Sven Laur University of Tartu

Modelling and Control of Dynamic Systems. Stability of Linear Systems. Sven Laur University of Tartu Modelling and Control of Dynamic Systems Stability of Linear Systems Sven Laur University of Tartu Motivating Example Naive open-loop control r[k] Controller Ĉ[z] u[k] ε 1 [k] System Ĝ[z] y[k] ε 2 [k]

More information

MASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Electrical Engineering and Computer Science : Dynamic Systems Spring 2011

MASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Electrical Engineering and Computer Science : Dynamic Systems Spring 2011 MASSACHUSETTS INSTITUTE OF TECHNOLOGY Department of Electrical Engineering and Computer Science 6.4: Dynamic Systems Spring Homework Solutions Exercise 3. a) We are given the single input LTI system: [

More information

Multivariable Control. Lecture 03. Description of Linear Time Invariant Systems. John T. Wen. September 7, 2006

Multivariable Control. Lecture 03. Description of Linear Time Invariant Systems. John T. Wen. September 7, 2006 Multivariable Control Lecture 3 Description of Linear Time Invariant Systems John T. Wen September 7, 26 Outline Mathematical description of LTI Systems Ref: 3.1-3.4 of text September 7, 26Copyrighted

More information

Observers for Linear Systems with Unknown Inputs

Observers for Linear Systems with Unknown Inputs Chapter 3 Observers for Linear Systems with Unknown Inputs As discussed in the previous chapters, it is often the case that a dynamic system can be modeled as having unknown inputs (e.g., representing

More information

Chapter 3. Tohru Katayama

Chapter 3. Tohru Katayama Subspace Methods for System Identification Chapter 3 Tohru Katayama Subspace Methods Reading Group UofA, Edmonton Barnabás Póczos May 14, 2009 Preliminaries before Linear Dynamical Systems Hidden Markov

More information

Linear dynamical systems with inputs & outputs

Linear dynamical systems with inputs & outputs EE263 Autumn 215 S. Boyd and S. Lall Linear dynamical systems with inputs & outputs inputs & outputs: interpretations transfer function impulse and step responses examples 1 Inputs & outputs recall continuous-time

More information

Eigenspaces. (c) Find the algebraic multiplicity and the geometric multiplicity for the eigenvaules of A.

Eigenspaces. (c) Find the algebraic multiplicity and the geometric multiplicity for the eigenvaules of A. Eigenspaces 1. (a) Find all eigenvalues and eigenvectors of A = (b) Find the corresponding eigenspaces. [ ] 1 1 1 Definition. If A is an n n matrix and λ is a scalar, the λ-eigenspace of A (usually denoted

More information

A proof of the Jordan normal form theorem

A proof of the Jordan normal form theorem A proof of the Jordan normal form theorem Jordan normal form theorem states that any matrix is similar to a blockdiagonal matrix with Jordan blocks on the diagonal. To prove it, we first reformulate it

More information

Grammians. Matthew M. Peet. Lecture 20: Grammians. Illinois Institute of Technology

Grammians. Matthew M. Peet. Lecture 20: Grammians. Illinois Institute of Technology Grammians Matthew M. Peet Illinois Institute of Technology Lecture 2: Grammians Lyapunov Equations Proposition 1. Suppose A is Hurwitz and Q is a square matrix. Then X = e AT s Qe As ds is the unique solution

More information

Definition (T -invariant subspace) Example. Example

Definition (T -invariant subspace) Example. Example Eigenvalues, Eigenvectors, Similarity, and Diagonalization We now turn our attention to linear transformations of the form T : V V. To better understand the effect of T on the vector space V, we begin

More information

Zeros and zero dynamics

Zeros and zero dynamics CHAPTER 4 Zeros and zero dynamics 41 Zero dynamics for SISO systems Consider a linear system defined by a strictly proper scalar transfer function that does not have any common zero and pole: g(s) =α p(s)

More information

Control Systems. Linear Algebra topics. L. Lanari

Control Systems. Linear Algebra topics. L. Lanari Control Systems Linear Algebra topics L Lanari outline basic facts about matrices eigenvalues - eigenvectors - characteristic polynomial - algebraic multiplicity eigenvalues invariance under similarity

More information

Linear Algebra (MATH ) Spring 2011 Final Exam Practice Problem Solutions

Linear Algebra (MATH ) Spring 2011 Final Exam Practice Problem Solutions Linear Algebra (MATH 4) Spring 2 Final Exam Practice Problem Solutions Instructions: Try the following on your own, then use the book and notes where you need help. Afterwards, check your solutions with

More information

Theory of Linear Systems Exercises. Luigi Palopoli and Daniele Fontanelli

Theory of Linear Systems Exercises. Luigi Palopoli and Daniele Fontanelli Theory of Linear Systems Exercises Luigi Palopoli and Daniele Fontanelli Dipartimento di Ingegneria e Scienza dell Informazione Università di Trento Contents Chapter. Exercises on the Laplace Transform

More information

Carleton College, winter 2013 Math 232, Solutions to review problems and practice midterm 2 Prof. Jones 15. T 17. F 38. T 21. F 26. T 22. T 27.

Carleton College, winter 2013 Math 232, Solutions to review problems and practice midterm 2 Prof. Jones 15. T 17. F 38. T 21. F 26. T 22. T 27. Carleton College, winter 23 Math 232, Solutions to review problems and practice midterm 2 Prof. Jones Solutions to review problems: Chapter 3: 6. F 8. F. T 5. T 23. F 7. T 9. F 4. T 7. F 38. T Chapter

More information

Disturbance Decoupling and Unknown-Input Observation Problems

Disturbance Decoupling and Unknown-Input Observation Problems Disturbance Decoupling and Unknown-Input Observation Problems Lorenzo Ntogramatzidis Curtin University of Technology, Australia MTNS - July 5-9, 2010 L. Ntogramatzidis (Curtin University) MTNS - July 5-9,

More information

LINEAR ALGEBRA 1, 2012-I PARTIAL EXAM 3 SOLUTIONS TO PRACTICE PROBLEMS

LINEAR ALGEBRA 1, 2012-I PARTIAL EXAM 3 SOLUTIONS TO PRACTICE PROBLEMS LINEAR ALGEBRA, -I PARTIAL EXAM SOLUTIONS TO PRACTICE PROBLEMS Problem (a) For each of the two matrices below, (i) determine whether it is diagonalizable, (ii) determine whether it is orthogonally diagonalizable,

More information

Chap. 3. Controlled Systems, Controllability

Chap. 3. Controlled Systems, Controllability Chap. 3. Controlled Systems, Controllability 1. Controllability of Linear Systems 1.1. Kalman s Criterion Consider the linear system ẋ = Ax + Bu where x R n : state vector and u R m : input vector. A :

More information

MATH 304 Linear Algebra Lecture 23: Diagonalization. Review for Test 2.

MATH 304 Linear Algebra Lecture 23: Diagonalization. Review for Test 2. MATH 304 Linear Algebra Lecture 23: Diagonalization. Review for Test 2. Diagonalization Let L be a linear operator on a finite-dimensional vector space V. Then the following conditions are equivalent:

More information

Designing Information Devices and Systems II Spring 2018 J. Roychowdhury and M. Maharbiz Discussion 6B

Designing Information Devices and Systems II Spring 2018 J. Roychowdhury and M. Maharbiz Discussion 6B EECS 16B Designing Information Devices and Systems II Spring 2018 J. Roychowdhury and M. Maharbiz Discussion 6B 1 Stability 1.1 Discrete time systems A discrete time system is of the form: xt + 1 A xt

More information

Linear Algebra, part 2 Eigenvalues, eigenvectors and least squares solutions

Linear Algebra, part 2 Eigenvalues, eigenvectors and least squares solutions Linear Algebra, part 2 Eigenvalues, eigenvectors and least squares solutions Anna-Karin Tornberg Mathematical Models, Analysis and Simulation Fall semester, 2013 Main problem of linear algebra 2: Given

More information

Solution of Linear State-space Systems

Solution of Linear State-space Systems Solution of Linear State-space Systems Homogeneous (u=0) LTV systems first Theorem (Peano-Baker series) The unique solution to x(t) = (t, )x 0 where The matrix function is given by is called the state

More information

33A Linear Algebra and Applications: Practice Final Exam - Solutions

33A Linear Algebra and Applications: Practice Final Exam - Solutions 33A Linear Algebra and Applications: Practice Final Eam - Solutions Question Consider a plane V in R 3 with a basis given by v = and v =. Suppose, y are both in V. (a) [3 points] If [ ] B =, find. (b)

More information

Solutions to Final Exam

Solutions to Final Exam Solutions to Final Exam. Let A be a 3 5 matrix. Let b be a nonzero 5-vector. Assume that the nullity of A is. (a) What is the rank of A? 3 (b) Are the rows of A linearly independent? (c) Are the columns

More information

Chapter 4 Euclid Space

Chapter 4 Euclid Space Chapter 4 Euclid Space Inner Product Spaces Definition.. Let V be a real vector space over IR. A real inner product on V is a real valued function on V V, denoted by (, ), which satisfies () (x, y) = (y,

More information

6.241 Dynamic Systems and Control

6.241 Dynamic Systems and Control 6.241 Dynamic Systems and Control Lecture 24: H2 Synthesis Emilio Frazzoli Aeronautics and Astronautics Massachusetts Institute of Technology May 4, 2011 E. Frazzoli (MIT) Lecture 24: H 2 Synthesis May

More information

Assignment 1 Math 5341 Linear Algebra Review. Give complete answers to each of the following questions. Show all of your work.

Assignment 1 Math 5341 Linear Algebra Review. Give complete answers to each of the following questions. Show all of your work. Assignment 1 Math 5341 Linear Algebra Review Give complete answers to each of the following questions Show all of your work Note: You might struggle with some of these questions, either because it has

More information

Observability. Dynamic Systems. Lecture 2 Observability. Observability, continuous time: Observability, discrete time: = h (2) (x, u, u)

Observability. Dynamic Systems. Lecture 2 Observability. Observability, continuous time: Observability, discrete time: = h (2) (x, u, u) Observability Dynamic Systems Lecture 2 Observability Continuous time model: Discrete time model: ẋ(t) = f (x(t), u(t)), y(t) = h(x(t), u(t)) x(t + 1) = f (x(t), u(t)), y(t) = h(x(t)) Reglerteknik, ISY,

More information

Linear Algebra Practice Problems

Linear Algebra Practice Problems Linear Algebra Practice Problems Page of 7 Linear Algebra Practice Problems These problems cover Chapters 4, 5, 6, and 7 of Elementary Linear Algebra, 6th ed, by Ron Larson and David Falvo (ISBN-3 = 978--68-78376-2,

More information

NORMS ON SPACE OF MATRICES

NORMS ON SPACE OF MATRICES NORMS ON SPACE OF MATRICES. Operator Norms on Space of linear maps Let A be an n n real matrix and x 0 be a vector in R n. We would like to use the Picard iteration method to solve for the following system

More information

Math 413/513 Chapter 6 (from Friedberg, Insel, & Spence)

Math 413/513 Chapter 6 (from Friedberg, Insel, & Spence) Math 413/513 Chapter 6 (from Friedberg, Insel, & Spence) David Glickenstein December 7, 2015 1 Inner product spaces In this chapter, we will only consider the elds R and C. De nition 1 Let V be a vector

More information

Perspective. ECE 3640 Lecture 11 State-Space Analysis. To learn about state-space analysis for continuous and discrete-time. Objective: systems

Perspective. ECE 3640 Lecture 11 State-Space Analysis. To learn about state-space analysis for continuous and discrete-time. Objective: systems ECE 3640 Lecture State-Space Analysis Objective: systems To learn about state-space analysis for continuous and discrete-time Perspective Transfer functions provide only an input/output perspective of

More information

Matrix Operations: Determinant

Matrix Operations: Determinant Matrix Operations: Determinant Determinants Determinants are only applicable for square matrices. Determinant of the square matrix A is denoted as: det(a) or A Recall that the absolute value of the determinant

More information

MATH 304 Linear Algebra Lecture 20: Review for Test 1.

MATH 304 Linear Algebra Lecture 20: Review for Test 1. MATH 304 Linear Algebra Lecture 20: Review for Test 1. Topics for Test 1 Part I: Elementary linear algebra (Leon 1.1 1.4, 2.1 2.2) Systems of linear equations: elementary operations, Gaussian elimination,

More information

Chapter 2 Subspaces of R n and Their Dimensions

Chapter 2 Subspaces of R n and Their Dimensions Chapter 2 Subspaces of R n and Their Dimensions Vector Space R n. R n Definition.. The vector space R n is a set of all n-tuples (called vectors) x x 2 x =., where x, x 2,, x n are real numbers, together

More information

ECE504: Lecture 8. D. Richard Brown III. Worcester Polytechnic Institute. 28-Oct-2008

ECE504: Lecture 8. D. Richard Brown III. Worcester Polytechnic Institute. 28-Oct-2008 ECE504: Lecture 8 D. Richard Brown III Worcester Polytechnic Institute 28-Oct-2008 Worcester Polytechnic Institute D. Richard Brown III 28-Oct-2008 1 / 30 Lecture 8 Major Topics ECE504: Lecture 8 We are

More information

Math 4377/6308 Advanced Linear Algebra

Math 4377/6308 Advanced Linear Algebra 2.4 Inverse Math 4377/6308 Advanced Linear Algebra 2.4 Invertibility and Isomorphisms Jiwen He Department of Mathematics, University of Houston jiwenhe@math.uh.edu math.uh.edu/ jiwenhe/math4377 Jiwen He,

More information

16.31 Fall 2005 Lecture Presentation Mon 31-Oct-05 ver 1.1

16.31 Fall 2005 Lecture Presentation Mon 31-Oct-05 ver 1.1 16.31 Fall 2005 Lecture Presentation Mon 31-Oct-05 ver 1.1 Charles P. Coleman October 31, 2005 1 / 40 : Controllability Tests Observability Tests LEARNING OUTCOMES: Perform controllability tests Perform

More information

Large Scale Data Analysis Using Deep Learning

Large Scale Data Analysis Using Deep Learning Large Scale Data Analysis Using Deep Learning Linear Algebra U Kang Seoul National University U Kang 1 In This Lecture Overview of linear algebra (but, not a comprehensive survey) Focused on the subset

More information

2 b 3 b 4. c c 2 c 3 c 4

2 b 3 b 4. c c 2 c 3 c 4 OHSx XM511 Linear Algebra: Multiple Choice Questions for Chapter 4 a a 2 a 3 a 4 b b 1. What is the determinant of 2 b 3 b 4 c c 2 c 3 c 4? d d 2 d 3 d 4 (a) abcd (b) abcd(a b)(b c)(c d)(d a) (c) abcd(a

More information

Math 313 Chapter 5 Review

Math 313 Chapter 5 Review Math 313 Chapter 5 Review Howard Anton, 9th Edition May 2010 Do NOT write on me! Contents 1 5.1 Real Vector Spaces 2 2 5.2 Subspaces 3 3 5.3 Linear Independence 4 4 5.4 Basis and Dimension 5 5 5.5 Row

More information