CN112149273A - Fast-convergence alternating current power grid distributed state estimation method - Google Patents

Fast-convergence alternating current power grid distributed state estimation method Download PDF

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CN112149273A
CN112149273A CN202010830082.8A CN202010830082A CN112149273A CN 112149273 A CN112149273 A CN 112149273A CN 202010830082 A CN202010830082 A CN 202010830082A CN 112149273 A CN112149273 A CN 112149273A
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陈博
胡明南
石家宇
翁世清
俞立
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Zhejiang University of Technology ZJUT
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Abstract

A fast convergence AC power grid distributed state estimation method comprises the following steps: 1) providing a mathematical model of the alternating current network system, and providing a measurement model under the mixed use condition of the SCADA measuring instrument and the PMU measuring instrument; 2) dividing a power grid system into a plurality of areas according to actual conditions, and providing a measurement model of each power grid area; 3) converting the nonlinear least square problem into an iterative linear least square problem by using a Gauss-Newton method to solve; 4) a nonlinear distributed state estimation method which is only communicated with neighbors and can be converged quickly is designed through a distributed linear least square method constructed based on the block matrix inversion idea. The invention can quickly calculate the state estimation value so as to find out the state abnormity in time, and greatly reduces the communication times while ensuring the estimation performance of the system; in addition, local original measurement information and a local state estimation value do not need to be exchanged, and the privacy of power grid users is protected to the greatest extent.

Description

Fast-convergence alternating current power grid distributed state estimation method
Technical Field
The invention relates to the field of distributed alternating current power grid state estimation, in particular to a fast convergence method based on nonlinear least square, which is applied to an alternating current power grid and solves the state estimation problem of a large-scale distributed system.
Background
The grid system is a large complex network formed by connecting hundreds of power buses. A conventional centralized power grid system is usually configured with a central dispatching center, and a Data Acquisition and monitoring (SCADA) system and a Phasor Measurement Unit (PMU) manage Measurement and Control signals of the whole power grid system. In order to monitor whether the power grid operates stably, a state estimator is usually installed in a central dispatching center, the state estimator estimates the current state of the power grid system according to measured data of the power grid, and the dispatching center can judge whether the operation of the power grid system is abnormal according to the state, or can control the dispatching of the power by taking the state as the input quantity of a controller in the power grid system. However, with the increase of the demand of electricity, the scale of the power grid becomes larger and larger, and the access of new energy power generation leads the power plant to be dispersed more and more in space, which makes the defects of high calculation cost, high communication delay, poor fault tolerance and the like of the centralized power grid more and more prominent. Therefore, distributed power grid systems with lower calculation and communication costs and higher robustness are receiving more and more attention.
The distributed power grid system is generally divided into a plurality of areas according to geographical positions or by using a clustering algorithm, wherein the areas where line connection exists are neighbor areas. In the distributed system, each area is designed to converge on a distributed state estimator of a centralized state estimation result through local measurement information and key data provided by a neighbor area, and power scheduling of the area is controlled according to the state estimation result. However, in the ac power grid, the measurement and the state of the system have a non-linear relationship, so that it is difficult to perform distributed decomposition, which brings difficulty to the design of the distributed state estimator. On the other hand, because the power grid system is large in scale, the jacobian matrix constructed through topological information is usually ill-conditioned, so that the convergence rate of the traditional distributed state estimation method based on matrix inversion design is very slow, and the control difficulty of each link in the power grid system is increased. On the premise of considering network scale and computational efficiency, it is still challenging to design a fast-convergence distributed state estimation method for a large-scale alternating-current power grid system.
Disclosure of Invention
In order to solve the problem of slow state estimation convergence rate in a large-scale distributed alternating current power grid system, the invention provides a fast-convergence alternating current power grid distributed state estimation method.
The technical scheme adopted by the invention for solving the technical problems is as follows:
a fast convergence AC power grid distributed state estimation method comprises the following steps:
1) establishing an alternating current power grid measuring model;
defining the voltage of a bus i in a power grid as ViPhase angle of voltage is thetaiThe resistance on the line between bus i and bus j is rijReactance is xijConductance is gijSusceptance ofijThe shunt conductance between bus i and ground is
Figure RE-GDA0002749377430000021
Shunt susceptance of
Figure RE-GDA0002749377430000022
Shunt admittance of
Figure RE-GDA0002749377430000023
The shunt admittance on the transmission line between buses is
Figure RE-GDA0002749377430000024
Let the state x of the gridi=[Vi θi]TIf the shunt conductance and shunt susceptance of each bus in the power grid and the resistance and reactance of the transmission line between the buses are known, the measurement model of the alternating current power grid at the time k is
Figure RE-GDA0002749377430000025
Wherein u isii(k),uij(k) Measuring noise for zero mean gaussian; z is a radical ofii(k) Is a direct measurement of the bus voltage and the phase angle of the voltage, and when the measuring instrument is a SCADA instrument, only the bus voltage, namely C, can be measuredi=[1 0]When the measuring instrument is a PMU instrument, it can measure voltage and voltage phase angle, i.e.
Figure RE-GDA0002749377430000026
zij(k) Is to the active power P of the transmission lineij(k) And reactive power Qij(k) Is measured by a factor of hij(xi(k),xj(k))T=(Pij(k),Qij(k))TWherein, in the step (A),
Figure RE-GDA0002749377430000027
wherein
Figure RE-GDA0002749377430000031
By extending the measurement equations of all buses and transmission lines, a global measurement model z (k) ═ h (x (k)) + u (k) is obtained, assuming that there are m measurements in the power grid, some
Figure RE-GDA0002749377430000032
2) Dividing a power grid distributed region;
dividing the power grid into a plurality of areas according to the geographical position of the power grid; each power grid region only has local parameter information and measurement data, and parameter information and measurement data on a connection line with an adjacent region; if the grid is divided into n regions, then global measurements are taken
Figure RE-GDA0002749377430000033
Wherein the measurement model of the region i is
Figure RE-GDA0002749377430000034
Wherein z isii(k) Is the bus i in the region1,...,ilMeasured value of, zij(k) For the region and the bus j connected in the region j1...jcMeasured values on the transmission line, which are respectively indicated as
Figure RE-GDA0002749377430000035
Figure RE-GDA0002749377430000036
Measuring noise of a measuring instrument in the area i; in general, formula (5) and formula (6) are collectively written as zi(k)=hi(x(k))+ui(k) (ii) a In addition, the area connected to the bus in the area i with the transmission line is defined as the neighborhood of the area i and is recorded as
Figure RE-GDA0002749377430000037
3) Designing a distributed state estimator;
estimating the state by taking the minimum mean square error of the residual error e (k) ═ z (k) — h (x (k)) as a criterion, namely solving the following minimization problem
Figure RE-GDA0002749377430000041
Wherein, the value of the state x (k) where the derivative of phi (x (k)) is zero is the estimation value to be evaluated, and let
Figure RE-GDA0002749377430000042
J (x (k)) is abbreviated as J (k); due to hi(k) The formula is a nonlinear equation, the above formula has no analytic solution, so that the iterative solution is carried out by using a Gauss-Newton method, and the formula of the p-th iteration is
Figure RE-GDA0002749377430000043
x(p+1)=x(p)+Δx(p), (10)
Wherein phi-1To estimate the error covariance matrix, equation (9) has the same form as the linear least squares estimation; however, in the distributed power grid system, each region only has measurement information of the region, and therefore, each region needs to use a distributed least square estimator to perform distributed solution on equation (9) to obtain a local state update value Δ xi(p) then passing xi(p+1)=xi(p)+Δxi(p) updating the local state;
4) designing a distributed nonlinear least square estimator;
the distributed estimator is divided into an inner loop part and an outer loop part according to the formula (9) and the formula (10), the inner loop part constructs a distributed linear least square method based on the block matrix inversion idea, and the outer loop part performs distributed iteration based on the Gauss-Newton method in the step 3).
Further, the process of the step 4) is as follows:
step 401, an outer loop initialization phase; setting an initial state estimation value of each node i
Figure RE-GDA0002749377430000044
Step 402, for an outer loop iteration round K1, 2i(k)=zi(k)-hi(k) And executing an inner loop (4.3) - (4.6);
step 403, an inner loop initialization phase; setting an initial estimation error covariance matrix of each node i to
Figure RE-GDA0002749377430000045
The linear estimate is
Figure RE-GDA0002749377430000046
For all neighbors
Figure RE-GDA0002749377430000047
Initialization settings
Figure RE-GDA0002749377430000048
Mij(0)=Mi(0);
Step 404, for an inner loop iteration round P1, 2
Figure RE-GDA0002749377430000049
Computing
Figure RE-GDA00027493774300000410
And will calculate the result betaij(p) and Ψij(p) to node j;
step 405, each node i receives the information sent by the neighbor node and updates
Figure RE-GDA0002749377430000051
Step 406, calculating a linear least squares estimate after inner loop convergence
Figure RE-GDA0002749377430000052
And is provided with
Figure RE-GDA0002749377430000053
Finishing the internal circulation;
step 407, after the inner loop is finished, each node i updates the state
Figure RE-GDA0002749377430000054
The technical conception of the invention is as follows: firstly, a mathematical model of an alternating current power grid system is given, and a measurement model under the condition that an SCADA measuring instrument and a PMU measuring instrument are mixed for use is given. And then, dividing the power grid system into a plurality of areas according to the actual situation, and providing a measurement model of each area power grid. And finally, designing a fast-convergence alternating current power grid distributed state estimation method, converting the nonlinear least square problem into an iterative linear least square problem by using a Gauss-Newton method, and designing a fast-convergence nonlinear distributed state estimation method only communicating with neighbors by using a distributed linear least square method constructed based on a block matrix inversion idea.
The invention has the following beneficial effects: by using a fast-convergence distributed state estimation method, early warning can be immediately given under the condition that the state is abnormal, and the method greatly reduces the communication times while ensuring the system performance; in addition, the method does not need to exchange local original measurement information and a local state estimation value, and the privacy of the power grid user is protected to the greatest extent.
Drawings
FIG. 1 is a schematic diagram of an IEEE 118-bus power grid distributed partitioning system;
FIG. 2 is a block diagram of a distributed state estimator;
fig. 3 is an inner loop iteration simulation diagram and an outer loop iteration estimation error simulation diagram.
Detailed Description
The invention is further described below with reference to the accompanying drawings.
Referring to fig. 1 to 3, a fast converging ac power grid distributed state estimation method includes the following steps:
1) establishing an alternating current power grid measuring model;
defining the voltage of each bus i in the power grid as ViPhase angle of voltage is thetaiThe resistance on the line between bus i and bus j is rijReactance is xijConductance is gijSusceptance ofijThe shunt conductance between bus i and ground is
Figure RE-GDA0002749377430000061
Shunt susceptance of
Figure RE-GDA0002749377430000062
Shunt admittance of
Figure RE-GDA0002749377430000063
The shunt admittance on the transmission line between buses is
Figure RE-GDA0002749377430000064
Let the state x of the gridi=[Vi θi]TIf the shunt conductance and shunt susceptance of each bus in the power grid and the resistance and reactance of the transmission line between the buses are known, the measurement model of the alternating current power grid at the time k is
Figure RE-GDA0002749377430000065
Wherein u isii(k),uij(k) Measuring noise for zero mean gaussian; z is a radical ofii(k) Is a direct measurement of the bus voltage and the phase angle of the voltage, and when the measuring instrument is a SCADA instrument, only the bus voltage, namely C, can be measuredi=[1 0]When the measuring instrument is a PMU instrument, it can measure voltage and voltage phase angle, i.e.
Figure RE-GDA0002749377430000066
zij(k) Is to the active power P of the transmission lineij(k) And reactive power Qij(k) Is measured by a factor of hij(xi(k),xj(k))T=(Pij(k),Qij(k))TWherein, in the step (A),
Figure RE-GDA0002749377430000067
wherein
Figure RE-GDA0002749377430000068
By extending the measurement equations of all buses and transmission lines, a global measurement model z (k) ═ h (x (k)) + u (k) is obtained, assuming that there are m measurements in the power grid, some
Figure RE-GDA0002749377430000069
2) Dividing a power grid distributed region;
dividing the power grid into a plurality of regions according to the geographical position of the power grid, wherein each power grid region only has local parameter information and measurement data, and parameter information and measurement data on a connection line with an adjacent region; if the grid is divided into n regions, then global measurements are taken
Figure RE-GDA0002749377430000071
Wherein the measurement model of the region i is
Figure RE-GDA0002749377430000072
Wherein z isii(k) Is the bus i in the region1,...,ilMeasured value of, zij(k) For the region and the bus j connected in the region j1...jcMeasured values on the transmission line, which are respectively indicated as
Figure RE-GDA0002749377430000073
Figure RE-GDA0002749377430000074
Measuring noise of a measuring instrument in the area i; in general, formula (5) and formula (6) are collectively written as zi(k)=hi(x(k))+ui(k) (ii) a In addition, the area connected to the bus in the area i with the transmission line is defined as the neighborhood of the area i and is recorded as
Figure RE-GDA0002749377430000075
3) Designing a distributed state estimator;
estimating the state by taking the minimum mean square error of the residual error e (k) ═ z (k) — h (x (k)) as a criterion, namely solving the following minimization problem
Figure RE-GDA0002749377430000076
Wherein, the value of the state x (k) where the derivative of phi (x (k)) is zero is the estimation value to be evaluated, and let
Figure RE-GDA0002749377430000077
For convenience of description, J (x (k)) is abbreviated as J (k); due to hi(k) The formula is a nonlinear equation, the above formula has no analytic solution, so that the iterative solution is carried out by using a Gauss-Newton method, and the formula of the p-th iteration is
Figure RE-GDA0002749377430000081
x(p+1)=x(p)+Δx(p), (24)
Wherein phi-1To estimate the error covariance matrix, equation (9) has the same form as the linear least squares estimation; however, in the distributed power grid system, each region only has measurement information of the region, and therefore, each region needs to use a distributed least square estimator to perform distributed solution on equation (9) to obtain a local state update value Δ xi(p) then passing xi(p+1)=xi(p)+Δxi(p) updating the local state;
4) designing a distributed least square estimator;
dividing the distributed estimator into an inner loop part and an outer loop part according to the formula (9) and the formula (10), wherein the inner loop part constructs a distributed linear least square method based on the block matrix inversion idea, and the outer loop part performs distributed iteration based on the Gauss-Newton method in the step 3);
the process of the step 4) is as follows:
step 401, an outer loop initialization phase; setting an initial state estimation value of each node i
Figure RE-GDA0002749377430000082
Step 402, for an outer loop iteration round K1, 2i(k)=zi(k)-hi(k) And executing an inner loop (4.3) - (4.6);
step 403, an inner loop initialization phase; setting an initial estimation error covariance matrix of each node i to
Figure RE-GDA0002749377430000083
The linear estimate is
Figure RE-GDA0002749377430000084
For all neighbors
Figure RE-GDA0002749377430000085
Initialization settings
Figure RE-GDA0002749377430000086
Mij(0)=Mi(0);
Step 404, for an inner loop iteration round P1, 2
Figure RE-GDA0002749377430000087
Computing
Figure RE-GDA0002749377430000088
And will calculate the result betaij(p) and Ψij(p) to node j;
step 405, each node i receives the information sent by the neighbor node and updates
Figure RE-GDA0002749377430000089
Step 406, calculating a linear least squares estimate after inner loop convergence
Figure RE-GDA00027493774300000810
And is provided with
Figure RE-GDA0002749377430000091
Finishing the internal circulation;
step 407, after the inner loop is finished, each node i updates the state
Figure RE-GDA0002749377430000092
With reference to fig. 3, firstly, the IEEE 118-bus grid system is divided into 8 areas according to fig. 1, and grid parameters are selected as CDF files provided by http:// labs.ece.uw.edu/pstca/pf118/pg _ tca118bus.htm; in addition, the voltage measurement error of the PMU measuring instrument is 0.002, the voltage angle measurement error is 0.01, the voltage measurement error and the power measurement error of the SCADA measuring instrument are 0.3, the circle in FIG. 1 represents a power bus, the 3 rd, 5 th, 9 th, 12 th, 15 th, 17 th, 21 th, 25 th, 28 th, 34 th, 37 th, 40 th, 45 th, 53 th, 56 th, 62 th, 64 th, 68 th, 76 th, 79 th, 85 th, 86 th, 89 th, 92 th, 96 th, 105 th, 110 th and 114 th buses are buses with PMU measurement, other buses are buses with the SCADA measuring instrument, and the connecting line between the circles is a transmission line between the buses; as shown in fig. 3, the simulation experiment starts with a certain initial deviation, each external iteration only needs 4 internal iterations to be basically stable, and the global estimation can be converged through 3 external iterations, so that the convergence rate is very high.

Claims (2)

1. A fast converging AC power grid distributed state estimation method is characterized by comprising the following steps;
1) establishing an alternating current power grid measuring model;
defining the voltage of a bus i in a power grid as ViPhase angle of voltage is thetaiThe resistance on the line between bus i and bus j is rijReactance is xijConductance is gijSusceptance ofijThe shunt conductance between bus i and ground is
Figure RE-FDA0002749377420000011
Shunt susceptance of
Figure RE-FDA0002749377420000012
Shunt admittance of
Figure RE-FDA0002749377420000013
The shunt admittance on the transmission line between buses is
Figure RE-FDA0002749377420000014
Let the state x of the gridi=[Vi θi]TIf the shunt conductance and shunt susceptance of each bus in the power grid and the resistance and reactance of the transmission line between the buses are known, the measurement model of the alternating current power grid at the time k is
Figure RE-FDA0002749377420000015
Wherein u isii(k),uij(k) Measuring noise for zero mean gaussian; z is a radical ofii(k) The voltage and the phase angle of the voltage on the bus are directly measured, and the measuring instrument is usedWhen the meter is a SCADA meter, only the bus voltage, i.e. C, can be measuredi=[1 0]When the measuring instrument is a PMU instrument, it can measure voltage and voltage phase angle, i.e.
Figure RE-FDA0002749377420000016
zij(k) Is to the active power P of the transmission lineij(k) And reactive power Qij(k) Is measured by a factor of hij(xi(k),xj(k))T=(Pij(k),Qij(k))TWherein, in the step (A),
Figure RE-FDA0002749377420000017
wherein
Figure RE-FDA0002749377420000018
By extending the measurement equations of all buses and transmission lines, a global measurement model z (k) ═ h (x (k)) + u (k) is obtained, assuming that there are m measurements in the power grid, some
Figure RE-FDA0002749377420000019
2) Dividing a power grid distributed region;
dividing the power grid into a plurality of areas according to the geographical position of the power grid; each power grid region only has local parameter information and measurement data, and parameter information and measurement data on a connection line with an adjacent region; if the grid is divided into n regions, then global measurements are taken
Figure RE-FDA00027493774200000110
Wherein the measurement model of the region i is
Figure RE-FDA00027493774200000111
Wherein z isii(k) Is the bus i in the region1,...,ilMeasured value of, zij(k) For the region and the bus j connected in the region j1...jcMeasured values on the transmission line, which are respectively indicated as
Figure RE-FDA0002749377420000021
Figure RE-FDA0002749377420000022
Figure RE-FDA0002749377420000023
Measuring noise of a measuring instrument in the area i; in general, formula (5) and formula (6) are collectively written as zi(k)=hi(x(k))+ui(k) (ii) a In addition, the area connected to the bus in the area i with the transmission line is defined as the neighborhood of the area i and is recorded as
Figure RE-FDA0002749377420000024
3) Designing a distributed state estimator;
estimating the state by taking the minimum mean square error of the residual error e (k) ═ z (k) — h (x (k)) as a criterion, namely solving the following minimization problem
argminφ(x(k))
Figure RE-FDA0002749377420000025
Wherein, the value of the state x (k) where the derivative of phi (x (k)) is zero is the estimation value to be evaluated, and let
Figure RE-FDA0002749377420000026
J (x (k)) is abbreviated as J (k); due to hi(k) The formula is a nonlinear equation, the above formula has no analytic solution, so that the iterative solution is carried out by using a Gauss-Newton method, and the formula of the p-th iteration is
Figure RE-FDA0002749377420000027
x(p+1)=x(p)+Δx(p), (10)
Wherein phi-1To estimate the error covariance matrix, equation (9) has the same form as the linear least squares estimation; however, in the distributed power grid system, each area only possesses the measurement information of the area, and therefore, each area needs to use the distributed least square estimator to perform distributed solution on equation (9) to obtain the local state update value Δ xi(p) then passing xi(p+1)=xi(p)+Δxi(p) updating the local state;
4) designing a distributed least square estimator;
the distributed estimator is divided into an inner loop part and an outer loop part according to the formula (9) and the formula (10), the inner loop part constructs a distributed linear least square method based on the block matrix inversion idea, and the outer loop part performs distributed iteration based on the Gauss-Newton method in the step 3).
2. The distributed state estimation method for an alternating current grid according to claim 1, characterized in that the procedure of step 4) is as follows:
4.1) an external circulation initialization stage; setting an initial state estimation value of each node i
Figure RE-FDA0002749377420000031
4.2) for the outer loop iteration round K1, 2i(k)=zi(k)-hi(k) And executing an inner loop (4.3) - (4.6);
4.3) an internal circulation initialization stage; is arranged at each timeThe initial estimation error covariance matrix of each node i is
Figure RE-FDA00027493774200000311
The linear estimate is
Figure RE-FDA0002749377420000032
For all neighbors
Figure RE-FDA0002749377420000033
Initialization settings
Figure RE-FDA0002749377420000034
Mij(0)=Mi(0);
4.4) for the inner loop iteration round P1, 2
Figure RE-FDA0002749377420000035
Computing
Figure RE-FDA0002749377420000036
And will calculate the result betaij(p) and Ψij(p) to node j;
4.5) each node i receives the information sent by the neighbor nodes and updates
Figure RE-FDA0002749377420000037
4.6) calculating the Linear least squares estimate after inner loop convergence
Figure RE-FDA0002749377420000038
And is provided with
Figure RE-FDA0002749377420000039
Finishing the internal circulation;
4.7) after the inner loop is finished, each node i updates the state
Figure RE-FDA00027493774200000310
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