Digital Control Systems (DCS)

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Digital Control Systems (DCS) Lecture-9-10 Modern Control Theory Dr. Imtiaz Hussain Associate Professor Mehran University of Engineering & Technology Jamshoro, Pakistan email: imtiaz.hussain@faculty.muet.edu.pk URL :http://imtiazhussainkalwar.weebly.com/ 7th Semester 14ES Note: I do not claim any originality in these lectures. The contents of this presentation are mostly taken from the book of Ogatta, Norman Nise, Bishop and B C. Kuo and various other internet sources.

Introduction The transition from simple approximate models, which are easy to work with, to more realistic models produces two effects. First, a large number of variables must be included in the models. Second, a more realistic model is more likely to contain nonlinearities and time-varying parameters. Previously ignored aspects of the system, such as interactions with feedback through the environment, are more likely to be included.

Introduction Most classical control techniques were developed for linear constant coefficient systems with one input and one output(perhaps a few inputs and outputs). The language of classical techniques is the Laplace or Z-transform and transfer functions. When nonlinearities and time variations are present, the very basis for these classical techniques is removed. Some successful techniques such as phase-plane methods, describing functions, and other methods, have been developed to alleviate this shortcoming.

Introduction The state variable approach of modern control theory provides a uniform and powerful methods of representing systems of arbitrary order, linear or nonlinear, with time-varying or constant coefficients. It provides an ideal formulation for computer implementation and is responsible for much of the progress in optimization theory. The advantages of using matrices when dealing with simultaneous equations of various kinds have long been appreciated in applied mathematics. The field of linear algebra also contributes heavily to modern control theory.

Introduction Conventional control theory is based on the input–output relationship, or transfer function approach. Modern control theory is based on the description of system equations in terms of n first-order differential equations, which may be combined into a first-order vector-matrix differential equation. The use of vector-matrix notation greatly simplifies the a mathematical representation of systems of equations. The increase in the number of state variables, the number of inputs, or the number of outputs does not increase the complexity of the equations.

State Space Representation State of a system: We define the state of a system at time t0 as the amount of information that must be provided at time t0, which, together with the input signal u(t) for t  t0, uniquely determine the output of the system for all t  t0. This representation transforms an nth order difference equation into a set of n 1st order difference equations. State Space representation is not unique. Provides complete information about all the internal signals of a system.

State Space Representation Suitable for both linear and non-linear systems. Software/hardware implementation is easy. A time domain approach. Suitable for systems with non-zero initial conditions. Transformation From Time domain to Frequency domain and Vice Versa is possible.

Definitions State Variable: The state variables of a dynamic system are the smallest set of variables that determine the state of the dynamic system. State Vector: If n variables are needed to completely describe the behaviour of the dynamic system then n variables can be considered as n components of a vector x, such a vector is called state vector. State Space: The state space is defined as the n-dimensional space in which the components of the state vector represents its coordinate axes.

Definitions Let x1 and x2 are two states variables that define the state of the system completely . State space of a Vehicle Two Dimensional State space State (t=t1) Velocity State (t=t1) State Vector Position

State Space Representation An electrical network is given in following figure, find a state-space representation if the output is the current through the resistor.

State Space Representation Step-1: Select the state variables. Step-2: Apply network theory, such as Kirchhoff's voltage and current laws, to obtain ic and vL in terms of the state variables, vc and iL. Applying KCL at Node-1 (1)

State Space Representation Step-2: Apply network theory, such as Kirchhoff's voltage and current laws, to obtain ic and vL in terms of the state variables, vc and iL. Applying KVL at input loop (2) Step-3: Write equation (1) & (2) in standard form. State Equations

State Space Representation

State Space Representation Step-4: The output is current through the resistor therefore, the output equation is

State Space Representation Where, x(t) --------------- State Vector A (nxn) ---------------- System Matrix B (nxp) ----------------- Input Matrix u(t) --------------- Input Vector Where, y(t) -------------- Output Vector C (qxn) ---------------- Output Matrix D ----------------- Feed forward Matrix

Example-1 Consider RLC Circuit Represent the system in Sate Space and find (if L=1H, R=3Ω and C=0.5 F): State Vector System Matrix Input Matrix & Input Vector Output Matrix & Output Vector Vc + - iL Vo Choosing vc and iL as state variables

Example-1 (cont...) State Equation Output Equation

Example-2 Consider the following system K M B x(t) M f(t) B Differential equation of the system is:

Example-2 As we know Choosing x and v as state variables

Example-2 If velocity v is the out of the system then output equation is given as

Example-3 Find the state equations of following mechanical translational system. System equations are:

Example-3 Now Choosing x1, v1, x2, v2 as state variables

Example-3 In Standard form

Example-3 In Vector-Matrix form

Example-3 If x1 and v2 are the outputs of the system then

Eigenvalues & Eigen Vectors The eigenvalues of an nxn matrix A are the roots of the characteristic equation. Consider, for example, the following matrix A:

Eigen Values & Eigen Vectors

Example#4 Find the eigenvalues if K = 2 M=10 B=3

Frequency Domain to time Domain Conversion Transfer Function to State Space K x(t) M f(t) B Differential equation of the system is: Taking the Laplace Transform of both sides and ignoring Initial conditions we get

The transfer function of the system is State Space Representation:

Draw a simulation diagram of equation (1) and (3) ……………………………. (1) ……………………………. (2) From equation (2) ……………………………. (3) Draw a simulation diagram of equation (1) and (3) -K/M -B/M F(s) 1/s 1/s X(s) P(s) 1/M

Let us assume the two state variables are x1 and x2. These state variables are represented in phase variable form as given below. -K/M -B/M 1/M F(s) 1/s 1/s X(s) P(s) State equations can be obtained from state diagram. The output equation of the system is

Example#5 Obtain the state space representation of the following Transfer function.

State Transition Any point P in state space represents the state of the system at a specific time t. State transitions provide complete picture of the system P(x1, x2) t0 t1 t2 t3 t4 t5 t6

Forced and Unforced Response Forced Response, with u(t) as forcing function Unforced Response (response due to initial conditions)

Solution of State Equations & State Transition Matrix Consider the state space model Solution of this state equation is given as Where is state transition matrix.

Example-1 Consider RLC Circuit Choosing vc and iL as state variables + - iL Vo

Example-1 (cont...)

Example-1 (cont...) State transition matrix can be obtained as Which is further simplified as

Example-1 (cont...) Taking the inverse Laplace transform of each element

End of Lectures-9-10 To download this lecture visit http://imtiazhussainkalwar.weebly.com/ End of Lectures-9-10