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Mathematical Modeling & Analysis PG Mechanical Engineering Design Module Lecture Slides: July-December 2013 Prof. (Dr.) Gaurang V. Shah Doctor of Engineering University of Massachusetts Lowell, USA Mechanical Engineering Department, PVPIT, Bavdhan Pune

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Page 1: Unit1 pg math model

Mathematical Modeling & Analysis

PG Mechanical Engineering Design ModuleLecture Slides: July-December 2013Prof. (Dr.) Gaurang V. Shah Doctor of EngineeringUniversity of Massachusetts Lowell, USAMechanical Engineering Department, PVPIT, Bavdhan Pune

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What is Mathematical Model?A set of mathematical equations (e.g., differential eqs.) that describes the input-output behavior of a system.

What is a model used for?

• Simulation

• Prediction/Forecasting

• Prognostics/Diagnostics

• Design/Performance Evaluation

• Control System Design

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Definition of SystemSystem: An aggregation or assemblage of things so combined by man or nature to form an integral and complex whole.

From engineering point of view, a system is defined as an interconnection of many components or functional units act together to perform a certain objective, e.g., automobile, machine tool, robot, aircraft, etc.

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To every system there corresponds three sets of variables:

Input variables originate outside the system and are not affected by what happens in the system

Output variables are the internal variables that are used to monitor or regulate the system. They result from the interaction of the system with its environment and are influenced by the input variables

Systemu y

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Dynamic SystemsA system is said to be dynamic if its current output may depend on the past history as well as the present values of the input variables. Mathematically,

Time : Input, :

]0),([)(

tu

tuty ≤τ≤τϕ=

Example: A moving mass

M

yu

Model: Force=Mass x Acceleration

uyM =

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Velocity-Force: ∫ ττ+==t

duM

ytytv0

)(1

)0()()(

Therefore, this is a dynamic system. If the drag force (bdx/dt) is included, then

uybyM =+

2nd order ordinary differential equation (ODE)

Position-Force:

dsduM

ytytyt s

∫ ∫ ττ++=0 0

)(1

)0()0()(

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Mathematical model of a real world system is derived using a combination of physical laws (1st principles) and/or experimental means

• Physical laws are used to determine the model structure (linear or nonlinear) and order.

• The parameters of the model are often estimated and/or validated experimentally.

• Mathematical model of a dynamic system can often be expressed as a system of differential (difference in the case of discrete-time systems) equations

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Input-output differential or difference equation

State equations (system of 1st order eqs.)

Transfer function

Nonlinear

Linear

Linear Time Invariant

System Type Model Type

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• A nonlinear model is often linearized about a certain operating point

• Model reduction (or approximation) may be needed to get a lumped-parameter (finite dimensional) model

• Numerical values of the model parameters are often approximated from experimental data by curve fitting.

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Differential Equations (Continuous-Time Systems)

ubububyayayay nnn

nnnn +++=++++ −

−−

− 1)1(

11)1(

1)(

)()1()()1()( 11 nkubkubnkyakyaky nn −++−+−++−=

Difference Equations (Discrete-Time Systems)

DiscretizationInverse Discretization

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Consider the mass-spring-damper (may be used as accelerometer or seismograph) system shown below:

Free-Body-Diagram

M

fs

fd

fs

fd

x

fs(y): position dependent spring force, y=x-ufd(y): velocity dependent spring force

Newton’s 2nd law ( ) )()( yfyfuyMxM sd −−=+=

Linearizaed model: uMkyybyM =++

M

ux

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Delayz -1

u y

Consider the digital system shown below:

Input-Output Eq.: )1()1()( −+−= kukyky

Equivalent to an integrator:

∑−

=

=1

0

)()(k

j

juky

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Transfer Function is the algebraic input-output relationship of a linear time-invariant system in the s (or z) domain

GU Y

dt

ds

kbsms

ms

sU

sYsGukyybym ≡

++==⇔=++ ,

)(

)()(

2

2

Example: Accelerometer System

Example: Digital Integrator

≡−

==⇔−+−= −

zz

z

zu

zYGkukyky ,

1)(

)()1()1()(

1

1 Forward shift

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• Transfer function is a property of the system independent from input-output signal

• It is an algebraic representation of differential equations

• Systems from different disciplines (e.g., mechanical and electrical) may have the same transfer function

• Chemical system of reacting species can be represented by TF

• Electromagnetic wave like LASER rep by TF(?).

PVPIT, 05/02/2013
CHEMICAL REACTION BETWEEN SPECIES CAN ALSO BE REPRESENTED BY TRANSFER FN..
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• Most systems in mechatronics are of the mixed type, e.g., electromechanical, hydromechanical, etc

• Each subsystem within a mixed system can be modeled as single discipline system first

• Power transformation among various subsystems are used to integrate them into the entire system

• Overall mathematical model may be assembled into a system of equations, or a transfer function

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voltage emf-backe,edt

diLiRu bb

aaaa =++=

Mechanical Subsystem BωωJTmotor +=

uia dc

Ra La

BInput: voltage uOutput: Angular velocity ω

Elecrical Subsystem (loop method):

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uia dc

Ra La

ω

Torque-Current:

Voltage-Speed:

atmotor iKT =

Combing previous equations results in the following mathematical model:

B

Power Transformation:

ωKe bb =

=+

=ω++

0at

baaa

a

iK-BωωJ

uKiRdt

diL

where Kt: torque constant, Kb: velocity constant For an ideal motor bt KK =

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Taking Laplace transform of the system’s differential equations with zero initial conditions gives:

Eliminating Ia yields the input-output transfer function

( ) btaaa2

a

t

KKBRBLJRJsL

K

U(s)

Ω(s)

++++=

uia Kt

Ra La

ω

B( )( )

=Ω+=Ω++

0)(

)()()(

sIK-(s)BJs

sUsKsIRsL

at

baaa

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Assuming small inductance, La ≈0

( )( )abt

at

RKKBJs

RK

U(s)

Ω(s)

++=

which is equivalent to

ωat RuK

Babt RKK

• The D.C. motor provides an input torque and an additional damping effect known as back-emf damping

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• A brushless PMSM has a wound stator, a PM rotor assembly and a position sensor.

• The combination of inner PM rotor and outer windings offers the advantages of– low rotor inertia– efficient heat dissipation, and – reduction of the motor size.

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a

qb

c

d

θe

θe=p θ+ θ0

Electrical angleNumber of poles/2

offset

θ

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qme

dmqq

dqmdd

vLL

Kipi

L

R

dt

di

vL

ipiL

R

dt

di

1

1

+ω−ω−−=

+ω+−=

Where p=number of poles/2, Ke=back emf constant

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• Parametric Identification: The input-output model coefficients are estimated to “fit” the input-output data.

• Frequency-Domain (non-parametric): The Bode diagram [G(jw) vs. w in log-log scale] is estimated directly form the input-output data. The input can either be a sweeping sinusoidal or random signal.

Experimental determination of system model. There are two methods of system identification:

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uia Kt

Ra La

ω

B

( )( ) 1+

=++

=Ts

k

RKKBJs

RK

U(s)

Ω(s)

abt

at

Transfer Function, La=0:

0 0.1 0.2 0.3 0.4 0.50

2

4

6

8

10

12

Time (secs)

Am

plitu

de

ku

T

u

t

k=10, T=0.1

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Graphical method is

• difficult to optimize with noisy data and multiple data sets

• only applicable to low order systems

• difficult to automate

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Given a linear system with uniformly sampled input output data, (u(k),y(k)), then

noisenkubkubnkyakyaky nn +−++−+−++−= )()1()()1()( 11

Least squares curve-fitting technique may be used to estimate the coefficients of the above model called ARMA (Auto Regressive Moving Average) model.

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Input: Random or deterministic

Random Noise

u

Output

n

plant

Noise model

• persistently exciting with as much power as possible;• uncorrelated with the disturbance • as long as possible

y

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• Analytical

• Experimental

– Time response analysis (e.g., step, impulse)

– Parametric

* ARX, ARMAX

* Box-Jenkins

* State-Space

– Nonparametric or Frequency based

* Spectral Analysis (SPA)

* Emperical Transfer Function Analysis (ETFE)

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Bode Diagram of

10-1

100

101

102

-10

0

10

20

Frequency (rad/sec)

Ga

in d

B

10-1

100

101

102

-30

-60

-90

0

Frequency (rad/sec)

Ph

ase

de

g

1/T

20log( )k

1)(

+=

Ts

ksG

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Method I (Sweeping Sinusoidal):

systemAiAo

f

t>>0

Magnitude Phasedb

=

=

A

Ai

0 , φ

Method II (Random Input):

system

Transfer function is determined by analyzing the spectrum of the input and output

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• Pointwise Estimation:)(

)()(

ωω=ω

U

YjG

This often results in a very nonsmooth frequency response because of data truncation and noise.

• Spectral estimation: uses “smoothed” sample estimators based on input-output covariance and crosscovariance.

The smoothing process reduces variability at the expense of adding bias to the estimate

)(ˆ)(ˆ

)(ˆωΦωΦ

u

yujeG

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0.1 1 10 100 1 10375

50

25

0

25

Frequency (Hz)

Ma

gn

itud

e (

dB

)

0.1 1 10 100 1 103180

90

0

90

180

Frequency (Hz)

Ph

ase (

Deg

)

high order

low order

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Neural Network Approach

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Prof. (Dr.) Gaurang ShahPVPIT, Pune

July-December 2013Lecture Notes: Mathematical Modeling Analysis PG ME (Design)

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IntroductionReal world nonlinear systems often difficult to

characterize by first principle modelingFirst principle models are often

suitable for control designModeling often accomplished with input-output maps

of experimental data from the systemNeural networks provide a powerful tool for data-

driven modeling of nonlinear systems

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])1[],...,[],1[],...,[(][ −−−−= kumkukymkygky

g

z -1 z -1 z -1

z -1 z -1 z -1

u

y

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• Artificial Neural Networks (ANN) are massively parallel computational machines (program or hardware) patterned after biological neural nets.

• ANN’s are used in a wide array of applications requiring reasoning/information processing including–pattern recognition/classification–monitoring/diagnostics–system identification & control–forecasting–optimization

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• Learning from examples rather than “hard” programming

• Ability to deal with unknown or uncertain situations

• Parallel architecture; fast processing if implemented in hardware

• Adaptability

• Fault tolerance and redundancy

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• Hard to design

• Unpredictable behavior

• Slow Training

• “Curse” of dimensionality

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• A neuron is a building block of biological networks

• A single cell neuron consists of the cell body (soma), dendrites, and axon.

• The dendrites receive signals from axons of other neurons.

• The pathway between neurons is synapse with variable strength

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Artificial Neural NetworksThey are used to learn a given input-output

relationship from input-output data (exemplars).Most popular ANNs:

Multilayer perceptronRadial basis functionCMAC

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Objective: Find a finite-dimensional representation of a function with compact domain

• Classical Techniques

-Polynomial, Trigonometric, Splines

• Modern Techniques

-Neural Nets, Fuzzy-Logic, Wavelets, etc.

mn RRAf →⊂:

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x1

x2

y

• MLP is used to learn, store, and produce input output relationships

Training: network are adjusted to match a set of known input-output (x,y) training data

Recall: produces an output according to the learned weights

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x y

Wk,ij: Weight from node i in layer k-1 to node j in layer k

( )( )( )( )xWσWσσWσWy TTTp

Tp 011 −=

σ: Activation function, e.g.,

+

+=

nx

x

e

e

1

1

1

1

)(1

W0 Wp

p: number of hidden layers

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A single hidden layer perceptron network with a sufficiently large number of neurons can approximate any continuous function arbitrarily close.

Comments:

• The UAT does not say how large the network should be

• Optimal design and training may be difficult

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Objective: Given a set of training input-output data (x,yt) FIND the network weights that minimize the expected error )yy(

2

tEL −=

Steepest Descent Method: Adjust weights in the direction of steepest descent of L to make dL as negative as possible.

tTdeEdL yye,0)y( −=≤=

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Examples:

• Cerebellar Model Articulation Controller (CMAC, Albus)

• B-Spline CMAC

• Radial Basis Functions

• Nodal Link Perceptron Network (NLPN, Sadegh)

These networks employ basis (or activation) functions that exist locally, i.e., they are activated only by a certain type of stimuli

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• Cerebellum: Responsible for complex voluntary movement and balance in humans

• Purkinje cells in cerebellar cortex is believed to have CMAC like architecture

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x y

)v,x(wy ii

ii∑ ϕ=

weightsbasis function

• One hidden layer only

• Local basis functions have adjustable parameters (vi’s)

• Each weight wi is directly related to the value of function at some x=xi

• similar to spline approximation

• Training algorithms similar to MLPs

wi

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Consider a function RRAf →⊂:

f(x) on interval [ai,ai+1] can be approximated by a lineai+1

wi

ai

wi+1

111

1)( +++

−+

−−= iii

ii

ii

i waa

axw

aa

axxf

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Defining the basis functions

)a,()( xwxfi

ii∑ ϕ=

∈−

−−

∈−−

=ϕ ++

−−

otherwise,0

],[,1

],[,

)( 11

11

1

iiii

i

iiii

i

i aaxaa

ax

aaxaa

ax

x

aiai-1 ai+1

Function f can expressed as

=

Na

a

1

a

This is also similar to fuzzy-logic approximation with “triangular” membership functions.

(1st order B-spline CMAC)

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Advantages of networks with local basis functions:

• Simpler to design and understand

• Direct Programmability

• Training is faster and localized

Main Disadvantage:

• Curse of dimensionality

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• Piecewise multilinear network (extension of 1-dimensional spline)

• Good approximation capability (2nd order)

• Convergent training algorithm

• Globally optimal training is possible

• Has been used in real world control applications

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x y

wi

)v,x(∑ ϕ=i

iiwy

)v,x()v,x()v,x()v,x( 21 21 niiii nϕϕϕ=ϕ

Input-Output Equation

Basis Function:

Each ϕ ij is a 1-dimensional triangular basis function over a finite interval

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y

y[k-m]

u[k-1]

Question: Is an arbitrary neural network model consistent with a physical system (i.e., one that has an internal realization)?

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])[x(][

])[],[x(f]1[x

khky

kukk

==+

u y

States: x1,…,xn

system

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A Class of Observable State Space Realizable Models

Consider the input-output model:

When does the input-output model have a state-space realization? :

])[x(][

])[],[x(f]1[x

khky

kukk

==+

])1[],...,[],1[],...,[(][ −−−−= kumkukymkygky

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• A Generic input-Output Model does not necessarily have a state-space realization (Sadegh 2001, IEEE Trans. On Auto. Control)

• There are necessary and sufficient conditions for realizability

• Once these conditions are satisfied the statespace model may be symbolically or computationally constructed

• A general class of input-Output Models may be constructed that is guaranteed to admit a state-space realization

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Prof. (Dr.) Gaurang ShahPVPIT, Pune

July-December 2013Lecture slideMathematical Modeling AnalysisPG

Mechanical Engineering (Design)

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APPLICATIONS:

Robotics Manufacturing Automobile industry Hydraulics

INTRODUCTION

EHPV control(electro-hydraulic poppet valve) Highly nonlinear Time varying characteristics Control schemes needed to

open two or more valves simultaneously

EXAMPLE:

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EXAMPLE:

Single EHPV learning control being investigated at Georgia Tech

Controller employs Neural Network in the feedforward loop with adaptive proportional feedback

Satisfactory results for single EHPV used for pressure control

INTRODUCTION

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IMPROVED CONTROL:

Linearized error dynamics - about (xd,k ,ud,k)

CONTROL DESIGN

( ) ( )kdkkkdkkdkkdnk o ,,,, , uueuuQeJe −+−+=+

kdkkkk ,1 ueJQu +−= −

Exact Control Law (deadbeat controller)

Nonlinear system (‘lifted’ to a square system)

( )kknk F uxx ,=+

Approximated Control Law

kkkkkk uueJQu ~~~1

11 ∆++−= −

−−

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IMPROVED CONTROL:

CONTROL DESIGN

kkkkkk uueJQu ~~~1

11 ∆++−= −

−−

Approximated Control Law

Estimation of Jacobian and controllability

Feedback correction

Nominal inverse mapping

inverse mapping correction

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