principles & applications of el t i l e i ielectrical...
TRANSCRIPT
Konkuk UniversityKonkuk University
Principles & Applications ofEl t i l E i iElectrical Engineering
Rizzoni, 5th Ed.
Ch 5 Transient Analysis
,
Ch. 5 Transient Analysis: first/second order circuits excited by switched DC source: provides general nature of D.E. solution method
ContentsContents Learning objectives
Understanding of transientsgSections 5.1.
Write differential equations for circuits containing q ginductors and capacitorsSections 5.2.
Determine the DC steady state solution of circuits containing inductors and capacitors Section 5.3.
Write differential equations of the first order circuits in standard form, and determine the complete solution of the first order circuits excited by switched DC sources
S ti 5 4
Dept. of Aerospace Information Engineering2
Section 5.4
Write differential equations of the second order circuits in standard form, and determine the complete solution pof second order circuits excited by switched DC sourcesSection 5.5
Understand analogies between electric circuits and hydraulic, thermal, and mechanical systems.y , , y
Dept. of Aerospace Information Engineering3
5.1 Transient analysis5.1 Transient analysis Transient analysis
Is to describe the behavior of a voltage or current during Is to describe the behavior of a voltage or current during the transition between two distinct steady state conditionsconditions
For instance, in the first order circuit,A decaying exponentialA decaying exponentialA rising exponential
1 0.368e
Dept. of Aerospace Information Engineering4
An exemplary representation of general R, L, C circuit with switched DC excitationThe required analysis is regarding ‘Transient
response’ using initial and final conditionsp g
Dept. of Aerospace Information Engineering5
5.2 Writing D.E. for circuit containing L and C5.2 Writing D.E. for circuit containing L and C Differential equations for circuits with dynamic
elementselements
vvdv
preferable1R
RCv
RCv
dtdv SCC
Dept. of Aerospace Information Engineering6
Exam 5.1Derive diff equation of the circuitDerive diff. equation of the circuit
Dept. of Aerospace Information Engineering7
p. 220 standard formulationp. 220 standard formulation First order system equation
Circuit containing only one dynamic elementCircuit containing only one dynamic elementComposed of time constant and DC gain
( ) ( )Sdx x t K f tdt
1 0 0( ) ( )dxa a x t b f tdt
Second order system equationCircuit containing two dynamic elementsg yComposed of natural frequency, damping ratio and DC
gaing2
2 2
1 2 ( ) ( )Sd x dx x t K f tdt dt
2
2 1 0 02 ( ) ( )d x dxa a a x t b f tdt dt
Dept. of Aerospace Information Engineering8
n ndt dt 0 02dt dt
Variables for first and second order D.E.Time constantTime constantDC gain
N t l fNatural frequencyDamping ratio
Dept. of Aerospace Information Engineering9
Exam 5.2Derive differential equation of RLC circuitDerive differential equation of RLC circuit
Use node voltage method and mesh current method, in orderin order
2
( ) ( )L Ld i diR CL R R C L R R i
Dept. of Aerospace Information Engineering10
1 1 2 1 22 ( ) ( )L LL SR CL R R C L R R i v
dt dt
5.3 DC steady state solution of circuits with Inductors and 5.3 DC steady state solution of circuits with Inductors and Capacitors Capacitors –– Initial and final conditionsInitial and final conditions
DC steady state solution of circuits with Inductors and Capacitorsand CapacitorsDC steady state solution provides the initial and final
conditions for the differential equationq
( ) ( )Sdx x t K f t Sx K f as t ( ) ( )S fdt S f
2 21 2 ( ) ( )Sd x d x x t K f t
x K f as t
The DC S S solution assumes steady state i e there
2 2 2 ( ) ( )Sn n
x t K f tdt dt
Sx K f as t
The DC S.S. solution assumes steady state, i.e., there is no change with respect to timeTime derivative of S.S solution zero
Dept. of Aerospace Information Engineering11
For capacitor case,steady state capacitor current by switched DC y p y
source( )( ) C
Cdv ti t C
dt
For inductor case
( ) 0C
dti t as t
For inductor case,steady state inductor voltage by switched DC source
( )di t( )( )
( ) 0
LL
L
di tv t Ldt
v t as t
At DC steady state, all capacitors behave as opencircuit and all inductors as short circuit
( )L
Dept. of Aerospace Information Engineering12
circuit and all inductors as short circuit.
Exam 5.4Determine the inductor current just before the switch isDetermine the inductor current just before the switch is
opened
Dept. of Aerospace Information Engineering13
‘Continuity’ of inductor current and capacitor voltagevoltage inductor current and capacitor voltage cannot change
instantaneously as this abrupt change will cause infiniteinstantaneously as this abrupt change will cause infinite amount of power.
This leads to the consequence thatThis leads to the consequence that Value of an inductor current or capacitor voltage just
prior to the closing (or opening) of a switch is equalprior to the closing (or opening) of a switch is equal to the value just after the switch has been closed (or opened)opened)
(0 ) (0 )C Cv v
Dept. of Aerospace Information Engineering14
(0 ) (0 )L Li i
Exam. 5.5 Initial and final value of inductor current? Initial and final value of inductor current?
Dept. of Aerospace Information Engineering15
5.4 Transient response of 15.4 Transient response of 1stst order D.E.order D.E. First order systems
ElectricalElectricalSingle dynamic element + resistor
H d liHydraulicFlow resistance + fluid capacitance (fluid mass
t )storage)Mechanical
Mass + dampingThermal
Storage + heat dissipation
Dept. of Aerospace Information Engineering16
Analogy in other engineering fieldHydraulic tankHydraulic tank
dq q q in out stored
out
q q qghqR
storeddhq Adt
h dh
( ) 0
gh dhAR dtRA dh h
( ) 0hg dt
Dept. of Aerospace Information Engineering17
5.4 Transient response of 15.4 Transient response of 1stst order D.E.order D.E. First order response
General form of D E ( ) ( )dx x t K f t General form of D.E.Assume the forced input is DC function (i.e.,f(t)=F)
N t l
( ) ( )Sx t K f tdt
Natural responseGiven when there exists no forced input
/
( ) ( ) 1( ) 0 ( )N NN N
dx t dx tx t x tdt dt
Forced response
/( ) tNx t e
pGiven when there exists a forced input of DC
( )dx t
Dept. of Aerospace Information Engineering18
( ) ( ) ( ) ( )FF S F S
dx t x t K F x t K F xdt
Complete responseComplete solution is sum of natural responseComplete solution is sum of natural response
(homogeneous solution) and forced response (particular solution)(particular solution)
( ) ( ) ( )N Fx t x t x t
f
In other form,
/( ) [ (0) ( )] ( )tx t x x e x ( ) [ (0) ( )] ( )x t x x e x
Dept. of Aerospace Information Engineering19
Example 5.7Find out capacitor voltage?Find out capacitor voltage?
Compute S.S. solution and initial condition Write D E and find time constant Write D.E. and find time constant Complete solution
/( ) [ (0) ( )] ( )t RC /( ) [ (0) ( )] ( )t RCC C C Cv t v v e v
Dept. of Aerospace Information Engineering20
Energy storage in capacitor and inductorCapacitorCapacitor
21( ) ( )W t Cv t
I d t
( ) ( )2 CCW t Cv t
Inductor
21( ) ( )W t Li t( ) ( )2L LW t Li t
Dept. of Aerospace Information Engineering21
/( ) tR LL Bi t I e
Equivalent circuit is considered to make a simple first order circuits, only when the action on switch is ybehaved.
Solve the capacitor voltage when switch is turned-on in the following figure.g g
Dept. of Aerospace Information Engineering22
After switched-on, we can use the equivalent circuit transformation as given belowg
Dept. of Aerospace Information Engineering23
Example 5.10Derive capacitor voltage equation?Derive capacitor voltage equation?
Switch closes at t=0, and open at t=50ms again. R1=R2=1k R3=500 R1 R2 1k, R3 500
1( ) ( ) [ (0) ( )] 0 50 sect
v t v v v e t m
2
'
( ) ( ) [ (0) ( )] , 0 50 sec
( ') ( ) [ ( ' 0) ( )] , 0 ' 50 sec( ) ?
C C C Ct
C C C C
v t v v v e t m
v t v v t v e t t mv t
( ) ?Cv t
Dept. of Aerospace Information Engineering24
5.5 Transient response of 25.5 Transient response of 2ndnd order systemorder system Circuit containing RLC
elementselementsContaining both types of
energy storage elementsenergy storage elements 2 simple configuration
L d C i ll lL and C in parallel connection
Diff t t / h• Different current amp/phase
L and C in series connectionconnection
• Different voltage amp/phase
Dept. of Aerospace Information Engineering25
Derivation of 2nd order D.E of RLC circuitsApply three basic equationsApply three basic equations
( ) ( ) ( ) 0( ) ( ) ( ) 0
T T S Cv t R i t v ti t i t i t
( ) ( ) ( ) 0( ) ( ) 0
S C L
L C
i t i t i tv t v t
Dept. of Aerospace Information Engineering26
Further equation development( ) ( ) ( )v t v t dv t( ) ( ) ( ) ( ) 0
( )
T C CL
T
v t v t dv tC i tR dt
di t
( )( ) LC
di tv t Ldt
( ) ( ) ( )t di t di tL d
2
( ) ( ) ( )( ) ( )
( ) ( ) ( )
T L LL
T T
v t di t di tL dC L i tR R dt dt dt
v t d i t di tL
2
( ) ( ) ( ) ( )T L LL
T T
v t d i t di tLLC i tR dt R dt
2
2
( ) ( )( )) ( )C CTC
d v t dv tdv tL Lcf LC v tR dt dt R dt
Dept. of Aerospace Information Engineering27
T TR dt dt R dt
Solution of second order circuits (normal differential equation form)q )
2
2 1 0 02
( ) ( ) ( ) ( )d x t dx ta a a x t b f tdt dt
From an engineering point of view (standard form)dt dt
22 1
2
( ) ( )2 ( ) ( )nn sd x t dx t x t K f t
dt dt
Natural frequency : 0 2/n a a
Damping ratio : DC gain :
1 0 2
0 0
( / 2) 1//
a a aK b a
Dept. of Aerospace Information Engineering28
g0 0/sK b a
The coefficients in the second order differential equation characterizes the system dynamics in terms of q y yoscillation frequency, overshoot characteristics, time response to steady state, and steady state DC gain
Dept. of Aerospace Information Engineering29
Zeta characterizes the overshoot and transient characteristicsDamping coefficient
Dept. of Aerospace Information Engineering30
Natural response of second order system2 ( ) ( )d d
S l ti d t b ti l f
22 1
2
( ) ( )2 ( ) ( )nn sd x t dx t x t K f t
dt dt
Solution assumed to be an exponential form as( ) st
Nx t eBy substituting the solution into governing equation,
2 2 12 0nst st st
n s e s e e Then the characteristic polynomials is given by
nn
2 2 1 2 22 1 0 2 0n nn ns s s s
Then the natural response is obtained using the solution of the characteristic polynomial
n nn n
Dept. of Aerospace Information Engineering31
solution of the characteristic polynomial 1 2
1 2( ) s t s tNx t e e
where2 2 21 (2 ) 4 1
Roots of second order system obtained as three cases
2 2 21,2 (2 ) 4 1
2n n n n ns
Roots of second order system obtained as three casesReal and distinct roots:
O d d1
• Overdamped case
Real and repeated roots:C iti ll d d
1 • Critically damped case
Complex conjugate roots:U d d d
1
• Underdamped case
Dept. of Aerospace Information Engineering32
Overdamped solution2 2
1 2
( 1) ( 1)1 2
/ /
( ) n n n nt tN
t t
x t e e
e e
Critically damped solution
1 2e e
Critically damped solution/ /
1 2( ) t tNx t e te
Underdamped solution Underdamped solution2 2( 1 ) ( 1 )
1 2( ) n n n nj t j tNx t e e
Dept. of Aerospace Information Engineering33
In the underdamped case, for instance If the same coefficient If the same coefficient
2 21 1( ) ( )n nn j t j ttNx t e e e
22 cos( 1 )ntne t
Exponentially decaying envelope
Sinusoidal signal
p y y g p
Dept. of Aerospace Information Engineering34
Natural response of over-damped second order system 2 2( 1) ( 1)( ) t t system
1 2
( 1) ( 1)1 2
/ /1 2
( ) n n n nt tN
t t
x t e e
e e
Dept. of Aerospace Information Engineering35
Natural response of critically damped second order system / /order system / /
1 2( ) t tNx t e te
Dept. of Aerospace Information Engineering36
Natural response of under-damped second order systemsystem
2 2( 1 ) ( 1 )1 2( ) n n n nj t j t
Nx t e e
2 2( ) 2 cos( 1 )ntN nx t e t
Dept. of Aerospace Information Engineering37
Forced response2 ( ) ( )d x t dx t2 1
2
( ) ( )2 ( ) ( )nn sd x t dx t x t K f t
dt dt
In this chapter assume only DC input force case. ( )f t F( )( ) ( )F s
fx t x K F
Dept. of Aerospace Information Engineering38
Complete responseSum of natural response (homogeneous solution) andSum of natural response (homogeneous solution) and
forced response (particular solution)Overdamped case:Overdamped case:
2 2
( ) ( ) ( )N Fx t x t x t 2 2( 1) ( 1)
1 2 ( )n n n nt te e x
Critically damped case( ) ( ) ( )N N Fx t x t x t
/ /1 2 ( )
N N F
t te te x 1
n
Dept. of Aerospace Information Engineering39
Underdamped case
( ) ( ) ( )x t x t x t 2 2( 1 ) ( 1 )
1 2
( ) ( ) ( )
( )n n n n
N F
j t j t
x t x t x t
e e x
To obtain unknown variables of alpha1 and alpha2,I iti l diti f (t 0) d d i ti f (t 0) Initial condition of x(t=0) and derivative of x(t=0)need to be substituted into the solution form
Dept. of Aerospace Information Engineering40
Automotive suspensionBecause of road surfaceBecause of road surface
profile, there exists displacement in thedisplacement in the automotive body.
What would be theWhat would be the dynamic response in accordance with damper acco da ce t da pestate??
Derive differentialDerive differential equation
Dept. of Aerospace Information Engineering41
Time response of displacementThe governing equation and transient responseThe governing equation and transient response
2
2
( )( ) ( ) ( ) ( ) RoadRoad
dx td x t dx tm b kx t x t bdt dt dt
dt dt dt
Dept. of Aerospace Information Engineering42
Reminders Identify the objective of the circuit equation Identify the objective of the circuit equationObtain the steady state values
I iti l/fi l diti Initial/final conditionsDerive differential equationDetermine the solution formFix the constants and complete solution
Dept. of Aerospace Information Engineering43
Example 5.14Determine complete response by solving differentialDetermine complete response by solving differential
equation for the current initial assumption (0 ) 5[ ]v V initial assumption (0 ) 5[ ]Cv V
Dept. of Aerospace Information Engineering44
Steady state response Initial conditions Initial conditions
DC final states1 2
(0 )(0 ) , LL
dii c cdt
DC final statesDifferential equation
21
2
( ) ( )2 ( ) 0nSL L
LdVd i t di tLC i t C
dt dt dt
Write the complete solution
Solve for the constants using initial conditions
Dept. of Aerospace Information Engineering45
solution3 208.7 3 4791.3( ) 4.36 10 4.36 10 0t t
Li t e e t
Dept. of Aerospace Information Engineering46
Example 5.16Determine complete response by solving differentialDetermine complete response by solving differential
equation for the current Initially capacitor is charged such that (0 ) 5[ ]v V Initially, capacitor is charged such that (0 ) 5[ ]Cv V
Dept. of Aerospace Information Engineering47
Steady state response
Initial conditions
Differential equation2
2
( ) ( ) ( ) 0SL LL
dVd i t di tLC RC i t Cdt dt dt
Write the complete solution
Solve for the constants using initial conditions
Dept. of Aerospace Information Engineering48
Final solution200( ) 0.05 sin 400 0t
Li t e t t ( ) 0.05 sin 400 0Li t e t t
Dept. of Aerospace Information Engineering49
SummarySummary Summary
Write differential equations for circuits containing inductor and icapacitor
Applying Kirchhoff’s law and constitutive i-v relationship of inductor and capacitorinductor and capacitor
Determine the DC steady state solution of circuits containing inductors and capacitors DC S.S. condition says that inductor behaves as short circuit
and capacitor as open circuit Write differential equations of the first order circuits in standard
form, and determine complete solution of first order circuits excited by switched DC sourcesby switched DC sources Commonly characterized by 2 constants, DC gain and time
constant
Dept. of Aerospace Information Engineering50
SummarySummaryWrite differential equations of the second order circuits
in standard form, and determine complete solution of psecond order circuits excited by switched DC sourcesCommonly characterized by 3 constants, natural y y ,
frequency, damping ratio, and DC gain
Understand analogies between electric circuits, hydraulic, thermal, and mechanical system.hydraulic, thermal, and mechanical system.Use the same standard form of differential equation
Dept. of Aerospace Information Engineering51
ExerciseExercise Example 5.11
First order circuit for motorFirst order circuit for motorFind motor voltage, vm
Dept. of Aerospace Information Engineering52