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State Estimation 
Vipin Chandra Pandey
State Estimation 
 assigning a value to an unknown system state variable based on 
measurements from that system according to some criteria. 
The process involves imperfect measurements that are redundant and the 
process of estimating the system states is based on a statistical criterion that 
estimates the true value of the state variables to minimize or maximize the 
selected criterion. 
Most Commonly used criterion for State Estimator in Power System is the 
Weighted Least Square Criteria.
State & Estimate 
What’s A State? 
 The complete “solution” of the power system is known 
if all voltages and angles are identified at each bus. 
These quantities are the “state variables” of the system. 
Why Estimate? 
 Meters aren’t perfect. 
 Meters aren’t everywhere. 
 Very few phase measurements? 
 SE suppresses bad measurements and uses the 
measurement set to the fullest extent. 2-3
State variable & Input to estimator 
 In the Power System, The State Variables are the voltage Magnitudes and 
Relative Phase Angles at the System Nodes. 
 The inputs to an estimator are imperfect power system measurements of 
voltage magnitude and power, VAR, or ampere flow quantities. 
 The Estimator is designed to produce the “best estimate” of the system 
voltage and phase angles, recognizing that there are errors in the measured 
quantities and that they may be redundant measurements.
State Estimator output 
Bus voltages, branch flows, …(state variables) 
 Measurement error processing results 
 Provide an estimate for all metered quantities 
 Filter out small errors due to model approximations and 
measurement inaccuracies. 
 Detect and identify discordant measurements, the 
so- called bad data.
Case 1 Suppose we use M13 and M32 and further suppose that 
M13 and M32 gives us perfect readings of the flows on their 
respective transmission lines. 
M13=5 MW=0.05pu 
M32 =40 MW=0.40pu 
f13=1/x13*(1- 3 )=M13 = 0.05 
f32=1/x32*(3- 2)=M32 = 0.40 
Since 3=0 rad 
1/0.4*(1- 0 )= 0.05 
1/0.25*(0- 2) = 0.40 
1 =0.02 rad 
2 =-0.10 rad
Case1-Measurement with accurate meters) 
Bus1 
Only two of these meter 
readings are required to 
calculate the bus phase 
angles and all load and 
generation values fully. 
Bus2 
Bus3 
60 MW 
40 MW 
65 MW 
100 MW 
Per unit Reactances 
(100 MVA Base): 
X12=0.2 
X13=0.4 
X23=0.25 
M12 
M13 
M32 
Meter Location 5 MW 
35 MW
Case-2: use only M12 and M32. 
M12=62 MW=0.62pu 
M32 =37 MW=0.37pu 
f12=1/x12*(1- 2 )=M12 = 0.62 
f32=1/x32*(3- 2)=M32 = 0.37 
Since 3=0 rad 
1/0.2*(1- 2 )= 0.62 
1/0.25*(0- 2) = 0.37 
1 =0.0315 rad 
2 =-0.0925 rad
Bus1 
Bus2 
Bus3 
62 MW 
37 MW 
65 MW 
100 MW 
Per unit Reactances 
(100 MVA Base): 
X12=0.2 
X13=0.4 
X23=0.25 
M12 
M13 
M32 
6 MW (7.875MW) 
Meter Location 
35 MW 
Case2-result of system flow. (M12 & M32) 
Mismatch
Analysis of example 
• use the measurements to estimate system conditions. 
• Measurements of were used to calculate the angles at different 
buses by which all unmeasured power flows, loads, and 
generations can be calculated. 
• voltage angles as the state variables for the three- bus system since 
knowing them allows all other quantities to be calculated 
• If we can use measurements to estimate the “states” of the power 
system, then we can go on to calculate any power flows, 
generation, loads, and so forth that we desire.
Solution Methodologies 
Weighted Least Square (WLS)method: 
Minimizes the weighted sum of squares of the difference between 
measured and calculated values . 
 The weighted least-squares criterion, where the objective is to minimize 
the sum of the squares of the weighted deviations of the estimated measurements, z, 
from the actual measurements, z. 
m 
1 
e2 
2 i 
i 1 i 
Iteratively Reweighted Least Square 
Value (WLAV)method: 
(IRLS)Weighted Least Absolute 
 Minimizes the weighted sum of the absolute value of difference 
between measured and calculated values. 
The objective function to be minimized is given by 
m 
| pi| 
i 1 
The weights get updated in every iteration.
(Cont.,) 
 The measurements are assumed to be in error: that is, the value 
obtained from the measurement device is close to the true 
value of the parameter being measured but differs by an 
unknown error. 
 If Zmeas be the value of a measurement as received from a 
 measurement device. 
 If Ztrue be the true value of the quantity being measured. 
 Finally, let η be the random measurement error. 
Then mathematically it is expressed as 
푧푚푒푎푠 = 푧푡푟푢푒 + 휂
Probability density function 
The random number, η, serves to model the uncertainty in 
the measurements. 
If the measurement error is unbiased, the probability 
density function of η is usually chosen as a normal 
distribution with zero mean. 
푃퐷퐹 휂 = 
1 
휎 2휋 
∗ 푒(−휂 2 2휎2) 
where σ is called the standard deviation and σ^2 is called 
the variance of the random number. 
If σ is large, the measurement is relatively inaccurate (i.e., 
a poor-quality measurement device), whereas a small value 
of σ denotes a small error spread (i.e., a higher-quality 
measurement device).
Probability density function
Weighted least Squares-State Estimator 
min 퐽 푥 = 
푁푚 
푖=1 
푧푖 
푚푒푎푠 − 푓푖 푥 2 
휎푖 
2 
where 
fi = function that is used to calculate the value being 
measured by the ith measurement 
휎푖 
2 = variance for the ith measurement 
J(x) = measurement residual 
Nm = number of independent measurements 
zmeas= ith measured quantity. 
Note: that above equation may be expressed in per unit or 
in physical units such as MW, MVAR, or kV.
Estimate Ns unknown parameters using Nm 
measurements 
min 퐽(푥1, 푥2, 푥3, … , 푥푁푠, ) = 
푁푚 
푖=1 
푍푖 − 푓푖 푥1, 푥2, 푥3 , … , 푥푁푠 
2 /휎푖 
2 
Matrix Formulation: 
If the functions 푓푖 푥1, 푥2, … . , 푥푁푠 are linear functions. 
푓푖 푥1, 푥2, … . , 푥푁푠 = 푓푖 푥 = ℎ푖1푥1 + ℎ푖2푥2 +, … . , +ℎ푖푁푠 푥푁푠
In vector form f(x) 
 푓 푥 = 
푓1 푥 
푓2 푥 
. 
. 
푓푁푚(푥) 
= [퐻 푥 ] 
Where 
[H]=an Nm by Ns matrix containing the coefficients of the linear function 
[H]=measurement function coefficients matrix 
Nm= number of measurements 
Ns=number of unknown parameters being estimated 
 푍푚푒푎푠 = 
푧푚푒푎푠 
1 
푧푚푒푎푠 
2 
푧푚푒푎푠 
푁푚
min 퐽 푥 = [푧푚푒푎푠 − 푓 푥 ]푇 푅−1 [푧푚푒푎푠 
− 푓 푥 ] 
푅 = 
2 0 0 
0 ⋱ 0 
0 0 휎푁푚 
휎1 
2 
[R]=covariance matrix of measurement error 
min J x = {zmeas R−1 zmeas 
− xT H T R−1 zmeas − zmeasT 
R−1 H x 
+ xT H T R−1 H x}
The gradient of 훻퐽 푥 
훻퐽 푥 = −2 퐻 푇 푅−1 푧푚푒푎푠 + 2 퐻 푇 푅−1 퐻 푥 
훻퐽 푥 = 0 
푥푒푠푡 = [ 퐻 푇 푅−1 퐻 ]−1[퐻]푇 [푅−1]푧푚푒푎푠 
Case Ns<Nm over determined 
xest = [ H T R−1 H ]−1[H]T[R−1]zmeas 
Case Ns=Nm completely determined 
xest = [H]−1zmeas 
Case Ns>Nm underdetermined 
xest = [H]T[ H H T]−1zmeas
Weighted Least Squares-Example 
est 
1 
est 
2 
xest
(Cont.,) 
• To derive the [H] matrix, we need to write the measurements 
as a function of the state variables 
are written in per unit as 
1 2 . These functions and 
1 
M f ( ) 5 5 
12 12 1 2 1 2 
0.2 
1 
M f ( ) 2.5 
13 13 1 3 1 
0.4 
1 
M f ( ) 4 
32 32 3 2 2 
0.25
(Cont.,) 
5 5 
2.5 0 
0 4 
[H] 
2 
M12 
2 
M12 
2 
M13 
2 
M13 
2 
M32 
2 
M32 
0.0001 
R 0.0001 
0.0001
(Cont.,) 
• 
1 
1 
est 
1 
est 
2 
0.0001 5 5 
1 
2.5 0 
0 4 
5 2.5 0 
-5 0 -4 
0.0001 
0.0001 
0.0001 0.62 
0.06 
0.37 
5 2.5 0 
-5 0 -4 
0.0001 
0.0001
(Cont.,) 
• We get 
est 
1 
est 
2 
0.028571 
0.094286 
• From the estimated phase angles, we can calculate the power 
flowing in each transmission line and the net generation 
or load at each bus. 
5 ))2 (0.06 (2.5 ))2 (0.37 (4 ))2 
1 2 
0.0001 
2.14 
1 
0.0001 
2 
0.0001 
J( 1, 2 ) 
(0.62 (5
Solution of theweighted least square 
example
Application of State Estimation 
 To provide a view of real-time power system conditions 
 Real-time data primarily come from SCADA 
 SE supplements SCADA data: filter, fill, smooth. 
 To provide a consistent representation for power 
system security analysis 
• On-line dispatcher power flow 
• Contingency Analysis 
• Load Frequency Control 
 To provide diagnostics for modeling & maintenance
References 
Power generation operation and control by Allen J.Wood & 
Bruce F.Wollenberg 
Operation and control in Power systems by P.S.R. Murthy
THANK YOU

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State estimation

  • 1. State Estimation Vipin Chandra Pandey
  • 2. State Estimation  assigning a value to an unknown system state variable based on measurements from that system according to some criteria. The process involves imperfect measurements that are redundant and the process of estimating the system states is based on a statistical criterion that estimates the true value of the state variables to minimize or maximize the selected criterion. Most Commonly used criterion for State Estimator in Power System is the Weighted Least Square Criteria.
  • 3. State & Estimate What’s A State?  The complete “solution” of the power system is known if all voltages and angles are identified at each bus. These quantities are the “state variables” of the system. Why Estimate?  Meters aren’t perfect.  Meters aren’t everywhere.  Very few phase measurements?  SE suppresses bad measurements and uses the measurement set to the fullest extent. 2-3
  • 4. State variable & Input to estimator  In the Power System, The State Variables are the voltage Magnitudes and Relative Phase Angles at the System Nodes.  The inputs to an estimator are imperfect power system measurements of voltage magnitude and power, VAR, or ampere flow quantities.  The Estimator is designed to produce the “best estimate” of the system voltage and phase angles, recognizing that there are errors in the measured quantities and that they may be redundant measurements.
  • 5. State Estimator output Bus voltages, branch flows, …(state variables)  Measurement error processing results  Provide an estimate for all metered quantities  Filter out small errors due to model approximations and measurement inaccuracies.  Detect and identify discordant measurements, the so- called bad data.
  • 6. Case 1 Suppose we use M13 and M32 and further suppose that M13 and M32 gives us perfect readings of the flows on their respective transmission lines. M13=5 MW=0.05pu M32 =40 MW=0.40pu f13=1/x13*(1- 3 )=M13 = 0.05 f32=1/x32*(3- 2)=M32 = 0.40 Since 3=0 rad 1/0.4*(1- 0 )= 0.05 1/0.25*(0- 2) = 0.40 1 =0.02 rad 2 =-0.10 rad
  • 7. Case1-Measurement with accurate meters) Bus1 Only two of these meter readings are required to calculate the bus phase angles and all load and generation values fully. Bus2 Bus3 60 MW 40 MW 65 MW 100 MW Per unit Reactances (100 MVA Base): X12=0.2 X13=0.4 X23=0.25 M12 M13 M32 Meter Location 5 MW 35 MW
  • 8. Case-2: use only M12 and M32. M12=62 MW=0.62pu M32 =37 MW=0.37pu f12=1/x12*(1- 2 )=M12 = 0.62 f32=1/x32*(3- 2)=M32 = 0.37 Since 3=0 rad 1/0.2*(1- 2 )= 0.62 1/0.25*(0- 2) = 0.37 1 =0.0315 rad 2 =-0.0925 rad
  • 9. Bus1 Bus2 Bus3 62 MW 37 MW 65 MW 100 MW Per unit Reactances (100 MVA Base): X12=0.2 X13=0.4 X23=0.25 M12 M13 M32 6 MW (7.875MW) Meter Location 35 MW Case2-result of system flow. (M12 & M32) Mismatch
  • 10. Analysis of example • use the measurements to estimate system conditions. • Measurements of were used to calculate the angles at different buses by which all unmeasured power flows, loads, and generations can be calculated. • voltage angles as the state variables for the three- bus system since knowing them allows all other quantities to be calculated • If we can use measurements to estimate the “states” of the power system, then we can go on to calculate any power flows, generation, loads, and so forth that we desire.
  • 11. Solution Methodologies Weighted Least Square (WLS)method: Minimizes the weighted sum of squares of the difference between measured and calculated values .  The weighted least-squares criterion, where the objective is to minimize the sum of the squares of the weighted deviations of the estimated measurements, z, from the actual measurements, z. m 1 e2 2 i i 1 i Iteratively Reweighted Least Square Value (WLAV)method: (IRLS)Weighted Least Absolute  Minimizes the weighted sum of the absolute value of difference between measured and calculated values. The objective function to be minimized is given by m | pi| i 1 The weights get updated in every iteration.
  • 12. (Cont.,)  The measurements are assumed to be in error: that is, the value obtained from the measurement device is close to the true value of the parameter being measured but differs by an unknown error.  If Zmeas be the value of a measurement as received from a  measurement device.  If Ztrue be the true value of the quantity being measured.  Finally, let η be the random measurement error. Then mathematically it is expressed as 푧푚푒푎푠 = 푧푡푟푢푒 + 휂
  • 13. Probability density function The random number, η, serves to model the uncertainty in the measurements. If the measurement error is unbiased, the probability density function of η is usually chosen as a normal distribution with zero mean. 푃퐷퐹 휂 = 1 휎 2휋 ∗ 푒(−휂 2 2휎2) where σ is called the standard deviation and σ^2 is called the variance of the random number. If σ is large, the measurement is relatively inaccurate (i.e., a poor-quality measurement device), whereas a small value of σ denotes a small error spread (i.e., a higher-quality measurement device).
  • 15. Weighted least Squares-State Estimator min 퐽 푥 = 푁푚 푖=1 푧푖 푚푒푎푠 − 푓푖 푥 2 휎푖 2 where fi = function that is used to calculate the value being measured by the ith measurement 휎푖 2 = variance for the ith measurement J(x) = measurement residual Nm = number of independent measurements zmeas= ith measured quantity. Note: that above equation may be expressed in per unit or in physical units such as MW, MVAR, or kV.
  • 16. Estimate Ns unknown parameters using Nm measurements min 퐽(푥1, 푥2, 푥3, … , 푥푁푠, ) = 푁푚 푖=1 푍푖 − 푓푖 푥1, 푥2, 푥3 , … , 푥푁푠 2 /휎푖 2 Matrix Formulation: If the functions 푓푖 푥1, 푥2, … . , 푥푁푠 are linear functions. 푓푖 푥1, 푥2, … . , 푥푁푠 = 푓푖 푥 = ℎ푖1푥1 + ℎ푖2푥2 +, … . , +ℎ푖푁푠 푥푁푠
  • 17. In vector form f(x)  푓 푥 = 푓1 푥 푓2 푥 . . 푓푁푚(푥) = [퐻 푥 ] Where [H]=an Nm by Ns matrix containing the coefficients of the linear function [H]=measurement function coefficients matrix Nm= number of measurements Ns=number of unknown parameters being estimated  푍푚푒푎푠 = 푧푚푒푎푠 1 푧푚푒푎푠 2 푧푚푒푎푠 푁푚
  • 18. min 퐽 푥 = [푧푚푒푎푠 − 푓 푥 ]푇 푅−1 [푧푚푒푎푠 − 푓 푥 ] 푅 = 2 0 0 0 ⋱ 0 0 0 휎푁푚 휎1 2 [R]=covariance matrix of measurement error min J x = {zmeas R−1 zmeas − xT H T R−1 zmeas − zmeasT R−1 H x + xT H T R−1 H x}
  • 19. The gradient of 훻퐽 푥 훻퐽 푥 = −2 퐻 푇 푅−1 푧푚푒푎푠 + 2 퐻 푇 푅−1 퐻 푥 훻퐽 푥 = 0 푥푒푠푡 = [ 퐻 푇 푅−1 퐻 ]−1[퐻]푇 [푅−1]푧푚푒푎푠 Case Ns<Nm over determined xest = [ H T R−1 H ]−1[H]T[R−1]zmeas Case Ns=Nm completely determined xest = [H]−1zmeas Case Ns>Nm underdetermined xest = [H]T[ H H T]−1zmeas
  • 20. Weighted Least Squares-Example est 1 est 2 xest
  • 21. (Cont.,) • To derive the [H] matrix, we need to write the measurements as a function of the state variables are written in per unit as 1 2 . These functions and 1 M f ( ) 5 5 12 12 1 2 1 2 0.2 1 M f ( ) 2.5 13 13 1 3 1 0.4 1 M f ( ) 4 32 32 3 2 2 0.25
  • 22. (Cont.,) 5 5 2.5 0 0 4 [H] 2 M12 2 M12 2 M13 2 M13 2 M32 2 M32 0.0001 R 0.0001 0.0001
  • 23. (Cont.,) • 1 1 est 1 est 2 0.0001 5 5 1 2.5 0 0 4 5 2.5 0 -5 0 -4 0.0001 0.0001 0.0001 0.62 0.06 0.37 5 2.5 0 -5 0 -4 0.0001 0.0001
  • 24. (Cont.,) • We get est 1 est 2 0.028571 0.094286 • From the estimated phase angles, we can calculate the power flowing in each transmission line and the net generation or load at each bus. 5 ))2 (0.06 (2.5 ))2 (0.37 (4 ))2 1 2 0.0001 2.14 1 0.0001 2 0.0001 J( 1, 2 ) (0.62 (5
  • 25. Solution of theweighted least square example
  • 26. Application of State Estimation  To provide a view of real-time power system conditions  Real-time data primarily come from SCADA  SE supplements SCADA data: filter, fill, smooth.  To provide a consistent representation for power system security analysis • On-line dispatcher power flow • Contingency Analysis • Load Frequency Control  To provide diagnostics for modeling & maintenance
  • 27. References Power generation operation and control by Allen J.Wood & Bruce F.Wollenberg Operation and control in Power systems by P.S.R. Murthy