Modern Control Systems (MCS) Dr. Imtiaz Hussain Assistant Professor email:...

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Modern Control Systems (MCS) Dr. Imtiaz Hussain Assistant Professor email: [email protected] URL :http://imtiazhussainkalwar.weebly.co m/ Lecture-25-26 Modeling of Digital Control Systems 1

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Modern Control Systems (MCS)

Dr. Imtiaz HussainAssistant Professor

email: [email protected] :http://imtiazhussainkalwar.weebly.com/

Lecture-25-26Modeling of Digital Control Systems

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Lecture Outline

β€’ Sampling Theorem

β€’ ADC Model

β€’ DAC Model

β€’ Combined Models

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Sampling Theoremβ€’ Sampling is necessary for the processing of analog data

using digital elements.

β€’ Successful digital data processing requires that the samples reflect the nature of the analog signal and that analog signals be recoverable from a sequence of samples.

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Sampling Theoremβ€’ Following figure shows two distinct waveforms with

identical samples.

β€’ Obviously, faster sampling of the two waveforms would produce distinguishable sequences.

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Sampling Theoremβ€’ Thus, it is obvious that sufficiently fast sampling is a

prerequisite for successful digital data processing.

β€’ The sampling theorem gives a lower bound on the sampling rate necessary for a given band-limited signal (i.e., a signal with a known finite bandwidth)

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Sampling Theoremβ€’ The band limited signal with

β€’ can be reconstructed from the discrete-time waveform

β€’ if and only if the sampling angular frequency satisfies the condition

𝑓 βˆ— (𝑑 )= βˆ‘π‘˜=βˆ’βˆž

∞

𝑓 (𝑑 )𝛿(π‘‘βˆ’π‘˜π‘‡ )

πœ”π‘ >2πœ”π‘š

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Selection of Sampling Frequency

β€’ A given signal often has a finite β€œeffective bandwidth” beyond which its spectral components are negligible.

β€’ This allows us to treat physical signals as band limited and choose a suitable sampling rate for them based on the sampling theorem.

β€’ In practice, the sampling rate chosen is often larger than the lower bound specified in the sampling theorem.

β€’ A rule of thumb is to choose asπœ”π‘ =π‘˜πœ”π‘š ,5β‰€π‘˜β‰€10

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Selection of Sampling Frequency

β€’ The choice of depends on the application.

β€’ In many applications, the upper bound on the sampling frequency is well below the capabilities of state-of-the-art hardware.

β€’ A closed-loop control system cannot have a sampling period below the minimum time required for the output measurement; that is, the sampling frequency is upper-bounded by the sensor delay.

πœ”π‘ =π‘˜πœ”π‘š ,5β‰€π‘˜β‰€10

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Selection of Sampling Frequency

β€’ For example, oxygen sensors used in automotive air/fuel ratio control have a sensor delay of about 20 ms, which corresponds to a sampling frequency upper bound of 50 Hz.

β€’ Another limitation is the computational time needed to update the control.

β€’ This is becoming less restrictive with the availability of faster microprocessors but must be considered in sampling rate selection.

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Selection of Sampling Frequency

β€’ For a linear system, the output of the system has a spectrum given by the product of the frequency response and input spectrum.

β€’ Because the input is not known a priori, we must base our choice of sampling frequency on the frequency response.

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Selection of Sampling Frequency (1st Order Systems)

β€’ The frequency response of first order system is

β€’ where K is the DC gain and is the system bandwidth.

β€’ Time constant and 3db bandwidth relationship

𝐻 ( π‘—πœ” )= πΎπ‘—πœ” /πœ”π‘+1

πœ”π‘=1𝑇

𝑓 3𝑑𝑏=1

2πœ‹π‘‡

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Selection of Sampling Frequency (1st Order Systems)

-30

-25

-20

-15

-10

-5

0

Mag

nitu

de (dB

)

System: sysFrequency (rad/s): 0.33Magnitude (dB): -2.97

System: sysFrequency (rad/s): 2.31Magnitude (dB): -16.9

10-2

10-1

100

101

-90

-45

0

Pha

se (de

g)

Bode Diagram

Frequency (rad/s)

𝐺 (𝑠)= 13𝑠+1

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Selection of Sampling Frequency (1st Order Systems)

β€’ The frequency response amplitude drops below the DC level by a factor of about 10 at the frequency .

β€’ If we consider , the sampling frequency is chosen as

πœ”π‘ =π‘˜πœ”π‘ ,35 β‰€π‘˜β‰€70

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Selection of Sampling Frequency (2nd Order Systems)

β€’ The frequency response of second order system is

β€’ The bandwidth of the system is approximated by the damped natural frequency

β€’ Using a frequency of as the maximum significant frequency, we choose the sampling frequency as

πœ”π‘ =π‘˜πœ”π‘‘ ,35β‰€π‘˜β‰€70

2)/(1/2)(

nnj

KjH

21 nd

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Example-1β€’ Given a first-order system of bandwidth 10 rad/s, select a

suitable sampling frequency and find the corresponding sampling period.

β€’ We know

β€’ Choosing k=60

Solution

πœ”π‘=10π‘Ÿπ‘Žπ‘‘ /𝑠𝑒𝑐

πœ”π‘ =π‘˜πœ”π‘ ,35 β‰€π‘˜β‰€70

πœ”π‘ =60πœ”π‘=600π‘Ÿπ‘Žπ‘‘ /𝑠𝑒𝑐

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Example-1β€’ Corresponding sapling period is calculated as

𝑇=2πœ‹πœ”π‘ 

=2Γ—3141

600=0.01𝑠𝑒𝑐

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Example-2β€’ A closed-loop control system must be designed for a steady-

state error not to exceed 5 percent, a damping ratio of about 0.7, and an undamped natural frequency of 10 rad/s. Select a suitable sampling period for the system if the system has a sensor delay of 0.02 sec.

β€’ Let the sampling frequency be

Solution

πœ”π‘ β‰₯35πœ”π‘‘

2135 ns

27.011035 s

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Example-2

β€’ The corresponding sampling period is

β€’ A suitable choice is T = 20 ms because this is equal to the sensor delay.

srads / 95.249

𝑇 ≀2Γ—3141249.95

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Home Workβ€’ A closed-loop control system must be designed for a steady-

state error not to exceed 5 percent, a damping ratio of about 0.7, and an undamped natural frequency of 10 rad/s. Select a suitable sampling period for the system if the system has a sensor delay of 0.03 sec.

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Introductionβ€’ A common configuration of digital control system is shown in

following figure.

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ADC Modelβ€’ Assume that

– ADC outputs are exactly equal in magnitude to their inputs (i.e., quantization errors are negligible)

– The ADC yields a digital output instantaneously– Sampling is perfectly uniform (i.e., occur at a fixed rate)

β€’ Then the ADC can be modeled as an ideal sampler with sampling period T.

T

t

u*(t)

0 t

u(t)

0

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0 t

u*(t)

t

u(t)

0

T

t

Ξ΄T(t)

0

Γ— =

modulating pulse(carrier)

modulated wave

Modulation signal

u(t) u*(t)

0

* )()()(k

kTttutu

Sampling Process

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DAC Modelβ€’ Assume that

– DAC outputs are exactly equal in magnitude to their inputs.– The DAC yields an analog output instantaneously.– DAC outputs are constant over each sampling period.

β€’ Then the input-output relationship of the DAC is given by

𝑒 (π‘˜ )𝑍𝑂𝐻→

𝑒h (𝑑 )=𝑒 (π‘˜ ) ,π‘˜π‘‡ ≀ 𝑑≀ (π‘˜+1 )𝑇

u(k)u(t)

uh(t)

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DAC Modelβ€’ Unit impulse response of ZOH

β€’ The transfer function can then be obtained by Laplace transformation of the impulse response.

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DAC Modelβ€’ As shown in figure the impulse response is a unit pulse of

width T.

β€’ A pulse can be represented as a positive step at time zero followed by a negative step at time T.

β€’ Using the Laplace transform of a unit step and the time delay theorem for Laplace transforms,

L {𝑒 (𝑑)}=1𝑠

L {βˆ’π‘’(π‘‘βˆ’π‘‡ )}=βˆ’ π‘’βˆ’π‘‡π‘ 

𝑠

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DAC Model

β€’ Thus, the transfer function of the ZOH is

L {𝑒 (𝑑)}=1𝑠

L {βˆ’π‘’(π‘‘βˆ’π‘‡ )}=βˆ’ π‘’βˆ’π‘‡π‘ 

𝑠

𝐺𝑍𝑂𝐻 (𝑠)=1βˆ’π‘’βˆ’π‘‡π‘ 

𝑠

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

β€’ The cascade of a DAC, analog subsystem, and ADC is shown in following figure.

β€’ Because both the input and the output of the cascade are sampled, it is possible to obtain its z-domain transfer function in terms of the transfer functions of the individual subsystems.

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

β€’ Using the DAC model, and assuming that the transfer function of the analog subsystem is G(s), the transfer function of the DAC and analog subsystem cascade is

𝐺𝑍𝐴 (𝑠 )=𝐺𝑍𝑂𝐻(𝑠)𝐺(𝑠)

𝐺𝑍𝐴 (𝑠 )=1βˆ’π‘’βˆ’π‘‡π‘ 

𝑠𝐺(𝑠)

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

β€’ The corresponding impulse response is

β€’ The impulse response is the analog system step response minus a second step response delayed by one sampling period.

𝐺𝑍𝐴 (𝑠 )=1βˆ’π‘’βˆ’π‘‡π‘ 

𝑠𝐺(𝑠)

𝐺𝑍𝐴 (𝑠 )=𝐺(𝑠)  βˆ’𝐺(𝑠)  π‘’βˆ’π‘‡π‘ 

𝑠

𝐺𝑍𝐴 (𝑠 )=𝐺(𝑠)𝑠

βˆ’πΊ(𝑠)  π‘’βˆ’π‘‡π‘ 

𝑠

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

𝐺𝑍𝐴 (𝑠 )=𝐺(𝑠)𝑠

βˆ’πΊ(𝑠)  π‘’βˆ’π‘‡π‘ 

𝑠

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

β€’ Inverse Laplace yields

β€’ Where

𝐺𝑍𝐴 (𝑠 )=𝐺(𝑠)𝑠

βˆ’πΊ(𝑠)  π‘’βˆ’π‘‡π‘ 

𝑠

𝑔𝑍𝐴 (𝑑 )=𝑔𝑠(𝑑)βˆ’π‘”π‘ (π‘‘βˆ’π‘‡ )

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

β€’ The analog response is sampled to give the sampled impulse response

β€’ By z-transforming, we can obtain the z-transfer function of the DAC (zero-order hold), analog subsystem, and ADC (ideal sampler) cascade.

𝑔𝑍𝐴 (𝑑 )=𝑔𝑠(𝑑)βˆ’π‘”π‘ (π‘‘βˆ’π‘‡ )

𝑔𝑍𝐴 (π‘˜π‘‡ )=𝑔𝑠(π‘˜π‘‡ )βˆ’π‘”π‘ (π‘˜π‘‡ βˆ’π‘‡ )

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DAC, Analog Subsystem, and ADC CombinationTransfer Function

β€’ Z-Transform is given as

β€’ The * in above equation is to emphasize that sampling of a time function is necessary before z-transformation.

β€’ Having made this point, the equation can be rewritten more concisely as

𝑔𝑍𝐴 (π‘˜π‘‡ )=𝑔𝑠(π‘˜π‘‡ )βˆ’π‘”π‘ (π‘˜π‘‡ βˆ’π‘‡ )

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z {π‘”π‘ β‘βˆ—(𝑑) }

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z[Lβˆ’1 {𝐺(𝑠)𝑠 }

βˆ—]

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z[𝐺(𝑠 )𝑠 ]

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Example-3β€’ Find GZAS(z) for the cruise control system for the vehicle shown

in figure, where u is the input force, v is the velocity of the car, and b is the viscous friction coefficient.

β€’ The transfer function of system is given as

β€’ Re-writing transfer function in standard form

Solution

𝐺 (𝑠 )=𝑉 (𝑠)π‘ˆ (𝑠)

= 1𝑀𝑠+𝑏

𝐺 (𝑠)= 𝐾𝜏 𝑠+1

=𝐾 /πœπ‘ +1/𝜏

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Example-3

β€’ Where and β€’ Now we know

β€’ Therefore,

β€’ The corresponding partial fraction expansion is

𝐺 (𝑠 )𝑠

= 𝐾 /πœπ‘  (𝑠+1/𝜏 )

𝐺 (𝑠)= 𝐾 /πœπ‘ +1/𝜏

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z[𝐺(𝑠 )𝑠 ]

𝐺 (𝑠 )𝑠

=(𝐾𝜏 ) [πœπ‘  βˆ’ πœπ‘ +1 /𝜏 ]

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Example-3

β€’ Using the z-transform table, the desired z-domain transfer function is

𝐺𝑍𝐴𝑆 (𝑧 )=z(1βˆ’π‘§βˆ’1)Z[(𝐾𝜏 ){πœπ‘  βˆ’ πœπ‘ +1/𝜏 }]

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z[𝐾 {1π‘ βˆ’

1𝑠+1/𝜏 }]

𝐺𝑍𝐴𝑆 (𝑧 )= π‘§βˆ’1𝑧 [𝐾 { 𝑧

π‘§βˆ’1βˆ’

π‘§π‘§βˆ’π‘’βˆ’π‘‡ /𝜏 }]

𝐺𝑍𝐴𝑆 (𝑧 )=[𝐾 {1βˆ’ π‘§βˆ’1π‘§βˆ’π‘’βˆ’π‘‡ /𝜏 }]

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Example-3

𝐺𝑍𝐴𝑆 (𝑧 )=[𝐾 {1βˆ’ π‘§βˆ’1π‘§βˆ’π‘’βˆ’π‘‡ /𝜏 }]

𝐺𝑍𝐴𝑆 (𝑧 )=𝐾 π‘§βˆ’π‘’βˆ’ π‘‡πœ βˆ’π‘§+1

π‘§βˆ’π‘’βˆ’π‘‡ /𝜏

𝐺𝑍𝐴𝑆 (𝑧 )=𝐾 1βˆ’π‘’βˆ’ π‘‡πœ

π‘§βˆ’π‘’βˆ’π‘‡ /𝜏

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Example-4β€’ Find GZAS(z) for the vehicle position control system, where u is

the input force, y is the position of the car, and b is the viscous friction coefficient.

β€’ The transfer function of system is given as

β€’ Re-writing transfer function in standard form

Solution

𝐺 (𝑠 )= π‘Œ (𝑠)π‘ˆ (𝑠)

= 1𝑠(𝑀𝑠+𝑏)

𝐺 (𝑠)= 𝐾𝑠 (𝜏 𝑠+1)

=𝐾 /𝜏

𝑠(𝑠+1𝜏

)

𝑦𝑏 οΏ½Μ‡οΏ½

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Example-4

β€’ Where and β€’ Now we know

β€’ Therefore,

β€’ The corresponding partial fraction expansion is

𝐺 (𝑠 )𝑠

= 𝐾 /πœπ‘ 2(𝑠+1/𝜏 )

𝐺 (𝑠)= 𝐾 /𝜏

𝑠 (𝑠+1𝜏

)

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z[𝐺(𝑠 )𝑠 ]

𝐺 (𝑠 )𝑠

=𝐾 [ 1

𝑠2βˆ’πœπ‘ +

πœπ‘ +1/𝜏 ]

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Example-4β€’ The desired z-domain transfer function can be obtained as

𝐺𝑍𝐴𝑆 (𝑧 )=(1βˆ’ π‘§βˆ’1)Z𝐾 [ 1

𝑠2βˆ’πœπ‘ +

πœπ‘ +1/𝜏 ]

𝐺𝑍𝐴𝑆 (𝑧 )= π‘§βˆ’1𝑧

𝐾 [ 𝑧(π‘§βˆ’1)2

βˆ’πœ π‘§π‘§βˆ’1

+ 𝜏 π‘§π‘§βˆ’π‘’βˆ’π‘‡ /𝜏 ]

𝐺𝑍𝐴𝑆 (𝑧 )=𝐾 [ 1𝑧 βˆ’1

βˆ’πœ+𝜏 (π‘§βˆ’1)π‘§βˆ’π‘’βˆ’π‘‡ /𝜏 ]

𝐺𝑍𝐴𝑆 (𝑧 )=𝐾 [ (1βˆ’πœ+πœπ‘’βˆ’ π‘‡πœ )𝑧+[πœβˆ’π‘’βˆ’π‘‡πœ (𝜏+1)]

(π‘§βˆ’1)(π‘§βˆ’π‘’βˆ’π‘‡ /𝜏 ) ]

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Example-5β€’ Find GZAS(z) for the series R-L circuit shown in Figure with

the inductor voltage as output.

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END OF LECTURES-25-26

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