Transfer Functions in Process Control: Definition, Development, and Properties, Study notes of Differential Equations

Transfer functions, their definition, development through an example, and their properties in the context of process control systems. Transfer functions are used to relate an input and output in a linear, dynamic model, enabling determination of the output response to any change in the input. The document also covers steady-state gain, order of a TF model, additive and multiplicative properties, and linearization of nonlinear models.

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Chapter 4
Transfer Functions
Convenient representation of a linear, dynamic model.
A transfer function (TF) relates one input and one output:
(
)
()
(
)
()
system
xt yt
Xs Ys
→→
The following terminology is used:
y
output
response
“effect”
x
input
forcing function
“cause”
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13
pf14
pf15
pf16
pf17
pf18
pf19
pf1a

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Download Transfer Functions in Process Control: Definition, Development, and Properties and more Study notes Differential Equations in PDF only on Docsity!

Transfer Functions

  • Convenient representation of a

linear

, dynamic model.

  • A transfer function (TF) relates

one

input and

one

output:

(^

(^

system

x t

y t

X

s^

Y

s

The following terminology is used:

y output response “effect”

x input forcing function “cause”

Definition of the transfer function: Let

G

(s

) denote the transfer function between an input,

x

, and an

output,

y

. Then, by definition

( )

(^

) ( ) Y

s

G s

X

s

where:

(^

)^

(^

)

( )

( )

Y

s

y t

X

s^

x t ^

^

^

^

L L

Development of Transfer Functions Example: Stirred Tank Heating System

Recall the previous dynamic model, assuming constant liquidholdup and flow rates:

(^

)^

i

dT

V

C

wC T

T

Q

dt

Suppose the process is initially at steady state:

(^

)^

(^

)^

(^

)^

(^

)

,^

,^

i^

i

T

T

T

T

Q

Q

where

steady-state value of

T,

etc. For steady-state

conditions:

T

(^

)

i

wC T

T

Q

Subtract (3) from (1):

(^

)^

(^

)^

(^

)^

i^

i

dT

V

C

wC

T

T

T

T

Q

Q

dt

^

^

But,

(^

)^

because

is a constant

d T

T

dT

T

dt

dt

Thus we can substitute into (4-2) to get,

(^

)^

i

dT

V

C

wC T

T

Q

dt

′^

′^

′^

where we have introduced the following “

deviation variables

also called “perturbation variables”:

,^

,^

i^

i^

i

T

T

T

T

T

T

Q

Q

Q

′^

′^

Take

L

of (6):

( )

(^

)^

( )

(^

)^

(^

)

i

V

C

sT

s^

T

t^

wC T

s^

T

s^

Q

s

′^

′^

′^

′^

^

^

^

^

where two new symbols are defined:

(^

)

and

V

K

wC

ρ w

Transfer Function Between

and

Q

′^

T

Suppose

is constant at the steady-state value. Then, i T

Then we can substitute into

(10) and rearrange to get the desired TF:

( )

(^

)^

(^

)

i^

i^

i^

i

T

t^

T

T

t^

T

s

′^

(^

) ( )

T

s

K

Q

s

s

′^

′^

8

Transfer Function Between

and

T

′^

i T

Suppose that

Q

is constant at its steady-state value:

(^

)^

(^

)^

(^

)

Q t

Q

Q

t^

Q

s

′^

Thus, rearranging

(^

) ( )

i T

s

T

s^

s

′^

′^

Comments:1. The TFs in (12) and (13) show the

individual

effects of

Q

and

on

T

. What about

simultaneous

changes in both

Q

and

?i T

i T

Properties of Transfer Function Models 1. Steady-State Gain

The steady-state of a TF can be used to calculate the steady-state change in an output due to a steady-state change in theinput. For example, suppose we know two steady states for aninput,

u

, and an output,

y

. Then we can calculate the steady-

state gain,

K

, from:

2

1

2

1

y

y

K

u

u −

For a linear system,

K

is a constant. But for a nonlinear

system,

K

will depend on the operating condition

(

) ,^

u y

Calculation of

K

from the TF Model:

If a TF model has a steady-state gain, then:

(^

)

0 lim

s

K

G s

•^

This important result is a consequence of the Final ValueTheorem

-^

Note

: Some TF models do

not

have a steady-state gain (e.g.,

integrating process in Ch. 5)

Definition: The order of the TF is defined to be the order of the denominatorpolynomial. Note: The order of the TF is equal to the order of the ODE. Physical Realizability: For any physical system,

in (4-38). Otherwise, the system

response to a step input will be an impulse. This can’t happen. Example:

n

m ≥

0

1

0

and step change in

du

a y

b

b u

u

dt

3. Additive Property

Suppose that an output is influenced by two inputs and thatthe transfer functions are known:

(^

) ( )

( )

( ) ( )

( )

1

2

1

2

and

Y

s^

Y

s

G

s^

G

s

U

s^

U

s

Then the response to changes in both

and

can be written

as:

1 U

2 U

(^

)^

(^

)^

(^

)^

(^

)^

(^

)

1

1

2

2

Y

s^

G

s U

s

G

s U

s

The graphical representation (or

block diagram

) is:

G

( 1 s) G

( 2 s)

Y

(s

)

U

( 1 s) U

( 2 s)

Linearization of Nonlinear Models • So far, we have emphasized linear models which can be

transformed into TF models.

  • But most physical processes and physical models are nonlinear.
    • But over a small range of operating conditions, the behavior

may be approximately linear.

-^

Conclude

: Linear approximations can be useful, especially

for purpose of analysis.

  • Approximate linear models can be obtained analytically by a

method called “linearization”. It is based on a Taylor SeriesExpansion of a nonlinear function about a specified operatingpoint.

  • Consider a nonlinear, dynamic model relating two process

variables,

u

and

y

(^

) ,^

dy

f^

y u

dt

Perform a Taylor Series Expansion about

and

and

truncate after the first order terms,

u

u

y

y

(^

)^

(^

)

,^

,^

y^

y

f^

f

f^

u y

f^

u y

u

y

u

y

′^

where

and

. Note that the partial derivative

terms are actually constants because they have been evaluated atthe nominal operating point,Substitute (4-61) into (4-60) gives:

u

u

u

y

y

y

′^

(^

) ,^

u y

(^

) ,

y^

y

dy

f^

f

f^

u y

u

y

dt

u

y

′^

Combine (1) and (2),

i^

v

dh A

q

C

h

dt

Linearize

term,

(^

)

h

h

h

h

h

Or

h

h

h R

where:

R

h

h

h

h

′^

Substitute linearized expression (5) into (3):

i^

v

dh A

q

C

h

h

dt

R

^

^

^

The steady-state version of (3) is:

i^

v

q

C

h

Subtract (7) from (6) and let

, noting that

gives the linearized model:

i^

i^

i

q

q

q

′^

dh

dh

dt

dt

i

dh A

q

h

dt

R

′^

′^