CN107732973B - Inverter low-voltage ride-through control method for weak network far-end severe voltage fault - Google Patents

Inverter low-voltage ride-through control method for weak network far-end severe voltage fault Download PDF

Info

Publication number
CN107732973B
CN107732973B CN201711164118.8A CN201711164118A CN107732973B CN 107732973 B CN107732973 B CN 107732973B CN 201711164118 A CN201711164118 A CN 201711164118A CN 107732973 B CN107732973 B CN 107732973B
Authority
CN
China
Prior art keywords
voltage
inverter
current
dref
qref
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201711164118.8A
Other languages
Chinese (zh)
Other versions
CN107732973A (en
Inventor
袁辉
宋美艳
辛焕海
黄林彬
徐璐瑶
汪震
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhejiang University ZJU
Original Assignee
Zhejiang University ZJU
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhejiang University ZJU filed Critical Zhejiang University ZJU
Priority to CN201711164118.8A priority Critical patent/CN107732973B/en
Publication of CN107732973A publication Critical patent/CN107732973A/en
Application granted granted Critical
Publication of CN107732973B publication Critical patent/CN107732973B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • H02J3/382
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J3/00Circuit arrangements for ac mains or ac distribution networks
    • H02J3/12Circuit arrangements for ac mains or ac distribution networks for adjusting voltage in ac networks by changing a characteristic of the network load
    • H02J3/16Circuit arrangements for ac mains or ac distribution networks for adjusting voltage in ac networks by changing a characteristic of the network load by adjustment of reactive power
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J3/00Circuit arrangements for ac mains or ac distribution networks
    • H02J3/38Arrangements for parallely feeding a single network by two or more generators, converters or transformers
    • H02J3/46Controlling of the sharing of output between the generators, converters, or transformers
    • H02J3/48Controlling the sharing of the in-phase component
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J3/00Circuit arrangements for ac mains or ac distribution networks
    • H02J3/38Arrangements for parallely feeding a single network by two or more generators, converters or transformers
    • H02J3/46Controlling of the sharing of output between the generators, converters, or transformers
    • H02J3/50Controlling the sharing of the out-of-phase component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E40/00Technologies for an efficient electrical power generation, transmission or distribution
    • Y02E40/30Reactive power compensation

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Inverter Devices (AREA)

Abstract

The invention discloses an inverter low-voltage ride-through control method aiming at a weak network far-end severe voltage fault. When a serious voltage fault occurs at the far end of the weak network, the active current control target quantity and the reactive current control target quantity in the inverter are switched to be zero, then the active current control target quantity and the reactive current control target quantity of the inverter are designed to be input, transient transition is carried out, phase-locked loops, current inner loops and voltage feedforward parameters are optimized, and the stability and the dynamic control performance of the inverter during low-voltage ride through are improved. The invention can avoid the instability of the inverter when the far end under the weak network has serious voltage drop fault, can effectively recover the voltage at the inverter terminal and enable the inverter to inject certain active power for supporting the frequency of a power grid, and can be applied to realizing the low voltage ride through of the inverter system when the far end of a new energy power station grid-connected system which takes the inverter as an interface under the weak network has serious voltage fault.

Description

Inverter low-voltage ride-through control method for weak network far-end severe voltage fault
Technical Field
The invention relates to the technical field of electrical information, in particular to a low-voltage ride-through control method of an inverter aiming at a remote severe voltage fault of a weak network.
Background
With the access of a large amount of power generated by renewable energy sources such as photovoltaic energy, wind energy and the like to a power system, low-voltage ride-through capability is provided for the power generation grid connection of the renewable energy sources at home and abroad. In addition, during the voltage drop, the grid-connected guide rules require that a wind power plant and a photovoltaic power station inject reactive current in a certain proportion to the voltage drop to support the voltage of a power grid, and the residual capacity is sent out in an active mode to prevent the power grid from generating large active shortage to influence the frequency stability of the system.
Grid-connected guidance generally assumes that an alternating current power grid is a strong grid (i.e., a line inductance value is small), and requires that an inverter has a certain low-voltage ride-through capability. However, renewable energy grid connection in China has the characteristics of long distance, large scale and high concentration, and a weak power grid (namely a large line inductance value) is usually arranged on the power grid side. Different from a voltage drop fault at a near-end public connection point in a strong network, when the voltage drop fault occurs at a far-end power grid side in a weak power grid, the voltage drop at the end of an inverter is small under the influence of a high inductive reactance value of a line, and a typical low-voltage ride-through control strategy possibly has an inapplicable risk, so that the inverter has a new instability problem.
At present, researches on the low voltage ride through process of the inverter mainly focus on the aspects of small interference stability analysis and static stability analysis, and few researches are conducted on the aspect of designing a low voltage ride through control method suitable for the low voltage ride through fault of the inverter system under the weak grid when the far-end severe voltage drop fault occurs.
Disclosure of Invention
In order to solve the problems, the invention provides an inverter low-voltage ride-through control method aiming at the serious voltage fault of the far end of the weak grid, which can effectively recover the voltage of the inverter end and enable the inverter to inject certain active power for supporting the grid frequency.
The technical scheme of the invention comprises the following steps:
when a serious voltage fault occurs at the far end of the weak network, the active current in the inverter is controlled to a target value IdrefAnd a reactive current control target amount IqrefSwitching to zero, and designing the control target quantity I of the active current of the inverterdrefAnd a reactive current control target amount IqrefAnd inputting, performing transient transition, optimizing phase-locked loop, current inner loop and voltage feedforward parameters, and improving the stability and dynamic control performance of the inverter during low voltage ride through.
In the invention, when the voltage of the remote end of the weak network drops to 0.2p.u. or below, the remote end of the weak network is considered to be a serious voltage fault. The low voltage ride through is voltage ride through aiming at the weak network far end severe voltage fault scene.
The design inverter active current control target quantity IdrefAnd a reactive current control target amount IqrefInputting, and performing transient transition, specifically:
firstly, obtaining a reactive current amplitude reference value I 'by utilizing integral control'qrefSo as to realize the adjustment of the terminal voltage without difference and obtain the equivalent voltage E and the equivalent impedance X of the alternating current power grid by utilizing the recursive least square method for identificationAnd calculating to obtain an active current amplitude reference value I'dref
Then, adopting a discrete active disturbance rejection controller to carry out reactive current amplitude reference value I'qrefAnd an active current amplitude reference value I'drefProcessing to obtain active current control target quantity I for input inverterdrefAnd a reactive current control target amount IqrefTo implement a transient transition process.
Obtaining a reactive current amplitude reference value I 'by utilizing integral control'qrefSpecifically, the following formula is adopted:
I′qref=∫ki(Vt-Vtref)dt
wherein k isiIs an integral coefficient, I'qrefInjecting a reactive current amplitude reference value, V, for the invertertTo the inverter terminal voltage, VtrefFor reference to terminal voltage, 0.9pu is selected in the implementation, and t represents time.
The method for identifying and obtaining the equivalent voltage E and the equivalent impedance X of the alternating current power grid by using the recursive least square methodAnd calculating to obtain an active current amplitude reference value I'drefThe following method is specifically adopted:
1) establishing equivalent voltage E and equivalent impedance X of alternating current power gridThe equality relationship between:
Vtd=Vt=E-XIq
wherein, VtdIs d-axis voltage component of inverter terminal voltage, E is equivalent voltage of AC network, XFor equivalent inductive reactance of the AC mains, IqIs the q-axis current component of the filter inductor;
2) calculating a parameter vector theta (t) to be solved at the t moment by adopting the following formula:
Figure BDA0001475896060000021
in the formula, θ (t)) For the parameter vector to be determined at time t, θ (t) ═ E X]T(ii) a Theta (t-1) is a parameter vector at the t-1 moment; y (t) is an output vector at the time t, and y (t) is equal to the voltage component V of the inverter terminal d axis at the time ttdI.e. y (t) ═ Vtd(t),Vtd(t) V at time ttd,VtdObtained by adopting the calculation of the step 1) above,
Figure BDA0001475896060000023
for the measurement vector at the time t,
Figure BDA0001475896060000022
Iq(t) represents the q-axis current component of the filter inductor at time t, Id(t) represents the d-axis current component of the filter inductor at time t, Id(t-1) represents a d-axis current component of the filter inductor at the time of t-1; p (t) is an inverse matrix of the covariance at time t; p (t-1) is an inverse matrix of the covariance at the time t-1;
in the formula Id(t)-Id(t-1) is an additional perturbation term used to speed up the algorithm convergence speed so that the term converges rapidly to 0.
3) When a severe voltage drop fault occurs, identification is triggered.
If the parameter vector theta (t) to be solved does not satisfy max (theta (t) -theta (t-1) }<1e-3Repeating the step 2) to perform recursive calculation;
if the parameter vector theta (t) to be solved meets max (theta (t) -theta (t-1) }<1e-3Outputting a parameter vector theta (t) to be solved as an identification result, and obtaining the equivalent voltage E of the alternating current power grid and the equivalent inductive reactance X of the alternating current power grid in the identification result
4) Calculating an active current amplitude reference value I 'by adopting the following formula'dref
I′dref=0.8E/X
In specific implementation, the maximum allowable injection value I of the d-axis current component of the network side line inverterdmaxComprises the following steps:
Idmax=E/X
the discrete active disturbance rejection controller is adopted to carry out parameter on reactive current amplitudeTo be examined'qrefAnd an active current amplitude reference value I'drefProcessing to obtain active current control target quantity I for input inverterdrefAnd a reactive current control target amount IqrefThe following method is specifically adopted:
first, a discrete type active disturbance rejection controller of the following formula is established:
Figure BDA0001475896060000031
wherein v is1(t) is the output of the discrete active disturbance rejection controller, i.e. the expected track; v. of2(t) is v1(t) the derivative of (t), h represents the sampling step, t represents the t-th time interval with h, and r is the amplitude of the amplitude limiter; r is0And h0Are respectively a controller fhan (v)1(t)-v(t),v2(t),r0,h0) Internal gain parameter and step parameter, v (t) is output of discrete type active disturbance rejection controller, i.e. v1(t) a desired value; fhan (v)1(t)-v(t),v2(t),r0,h0) And (3) representing the fastest control comprehensive function, specifically adopting a book active disturbance rejection control technology: method page 69 of estimate controls to compensate for uncertainty factors.
The discrete type active disturbance rejection controller of the invention designs a smooth transition process autonomously, and solves the problem of overshoot which may occur in reference point tracking.
Then, the inverter injects an active current control target quantity IdrefAnd a reactive current control target amount IqrefAnd (3) transition process: reference value I 'of active current amplitude'drefAs input v (t), i.e. v (t) ═ I ', to a discrete active disturbance rejection controller'dref(t) the output processed by the discrete type active disturbance rejection controller is an active current control target quantity IdrefI.e. Idref(t)=v1(t); reference value I 'of reactive current amplitude'qrefAs an input v '(t), i.e. v' (t) ═ I ', of another discrete active disturbance rejection controller'qref(t), output v 'processed by a discrete active disturbance rejection controller'1(t) injecting reactive current as inverterControl target amount IqrefI.e. Iqref(t)=v′1(t)。
The phase-locked loop frequency band reduction helps to improve the system damping at low voltage ride through, but this results in poor phase-locked loop phase-locking effect. Considering that when a serious low-voltage fault occurs, the voltage of the inverter at the initial stage may oscillate due to sudden change of the voltage at the far end, and the damping of a system should be mainly improved; when the voltage of the inverter terminal is restored to a certain degree, the system stability is improved to a certain extent along with the injection of reactive current, and the performance of the phase-locked loop can be improved mainly.
The phase-locked loop, the current inner loop and the voltage feedforward parameter comprise phase-locked loop integral coefficient ki_pllAnd the proportionality coefficient kp_pllIntegral coefficient of inner loop of current ki_accAnd the proportionality coefficient kp_accVoltage feedforward coefficient afSpecifically, the following method is adopted for optimization:
a) self-adaptive optimization phase-locked loop parameters: using inverter terminal voltage amplitude signal VtThe phase-locked loop parameters are optimized in real time by adopting the following formula:
Figure BDA0001475896060000041
in the formula: i VtI is the absolute value of terminal voltage amplitude, kp_pll、ki_pllAre respectively a phase-locked loop proportional coefficient and an integral coefficient k 'before optimization'p_pll、k′i_pllRespectively obtaining an optimized phase-locked loop proportional coefficient and an optimized integral coefficient;
by the formula optimization, the bandwidth of the phase-locked loop can be reduced at the initial stage of voltage fault, the system damping is increased, the stability of the inverter system at the initial stage of fault is improved, and meanwhile, in the voltage recovery process, the bandwidth of the phase-locked loop is gradually increased, the tracking speed of the phase-locked loop is improved, and the dynamic performance is improved.
b) Optimizing current inner loop parameters: adjusting the current inner loop proportionality coefficient kp_ccAnd integral coefficient ki_accMake the current inThe loop frequency band is within the range of 300 Hz-350 Hz;
c) optimizing voltage feedforward link parameters: reducing voltage feedforward loop parameter afTo 0.002-0.1.
The invention has the beneficial effects that:
the method can avoid the instability of the inverter when the far end under the weak grid has serious voltage drop fault, can effectively recover the voltage at the inverter terminal and enable the inverter to inject certain active power for supporting the frequency of the power grid, and can be applied to realizing the low voltage ride through of the inverter system when the far end of a new energy power station grid-connected system which takes the inverter as an interface under the weak grid has serious voltage fault.
Drawings
Fig. 1 is a block diagram and equivalent circuit of a typical low voltage ride through control for an inverter of the present invention.
Fig. 2 is a block diagram of an improved low voltage control strategy for an inverter of the present invention.
FIG. 3 is a block diagram of the calculation flow of the recursive least squares algorithm of the present invention.
FIG. 4 shows an example of X in the simulation verification of the present inventionAnd when k is 4 and E is 0.2pu, the voltage response curve of the inverter terminal is obtained.
Fig. 5 is a response curve of inverter terminal voltage and output active power when the proposed novel low voltage ride through control strategy is adopted in simulation verification according to an embodiment of the present invention.
Detailed Description
The invention is described in further detail below with reference to the figures and the embodiments.
The principle of the invention is as follows:
a typical low voltage ride through control strategy of the inverter and its structure are shown in fig. 1, and the definitions and physical meanings of some variables are shown in table 1 below. The Low Voltage Ride-Through (LVRT) control strategy comprises the following steps: the current control link and the current dq axis control target quantity. The values of the main parameters of the system are shown in table 2.
TABLE 1 symbolic definition and description of partial system variables in the drawings of the present invention
Figure BDA0001475896060000051
A current control link dynamic mathematical model:
Figure BDA0001475896060000052
in the formula: the first term on the right of the equation is a conventional current inner loop PI control link, the second term on the right of the equation is a current feedforward compensation term, and the third term on the right of the equation is voltage feedforward.
The current dq axis control target amount is:
Figure BDA0001475896060000053
Figure BDA0001475896060000054
in the formula: i isqref0Control target quantity, V, for q-axis current in pre-fault control modetIs the inverter terminal voltage amplitude, k is the gain factor,
Figure BDA0001475896060000055
upper limit of d-axis current control target amount, ImaxThe inverter current capacity (taken as 1.22pu here without loss of generality).
Table 2 Simulink simulation parameters
Rated voltage/V of system 380
Rated frequency/Hz of system 50
System rated capacity/kVA 10
Filter inductance Lf/pu 0.15
Filter capacitor Cf/pu 0.05
Damping resistor Rd 0.1
Current inner loop parameter kp_acck i_acc 1、15
Phase-locked loop parameter kp_pll、ki_pll 80、3500
Feed forward gain coefficient af 40
The new low voltage control method provided by the invention is an improvement on the basis of a typical low voltage ride through control strategy, and as shown in fig. 2, the specific improvement comprises the following steps:
1) changing the q-axis current control target amount Iqref. When a remote severe voltage drop fault occurs, the q-axis current control target amount becomes 0. Generating inverter injection reactive current amplitude reference value I 'through an integration link'qref,I′qrefGenerating a q-axis current control target quantity I through a discrete active disturbance rejection controllerqref. The specific implementation steps comprise:
firstly, generating an inverter injection reactive current amplitude reference value I 'through an integration link'qrefThe following formula:
I′qref=∫ki(Vt-Vtref)dt (4)
in the formula, kiIs an integral coefficient, here taken as 5, VtInverter terminal voltage, VtrefFor reference terminal voltage, 0.9pu is chosen here. Integral control is used to achieve a dead regulation of the terminal voltage.
The discrete type active disturbance rejection controller has the following specific formula:
Figure BDA0001475896060000061
wherein v is1(t) referred to as the desired trajectory, i.e. the output of the controller, v2(t) is v1(t) derivative of; h represents a sampling step size; t represents the t-th time with h as a time interval; r is an amplitude limiting amplitude; r is0,h0The internal parameters of the controller are; v (t) is v1(t) desired value, i.e. input to the controller, where let v (t) be I'qref;fhan(v1(t)-v(t),v2(t),r0,h0) Representing the steepest control synthesis function.
2) Changing d-axis current control target quantity Idref. When a remote severe voltage drop fault occurs, the d-axis current control target amount becomes 0. By identifying the equivalent voltage E and the equivalent inductive reactance X of the remote power gridDetermining the maximum allowable value I of the injection current of the d-axis of the inverterdmaxDesigning the inverter to inject an active current amplitude reference value I'dref,I′drefGenerating a d-axis current control target quantity I through a discrete active disturbance rejection controllerdref. The specific implementation steps comprise:
firstly, the equivalent voltage E and the equivalent inductive reactance X of the remote power grid need to be identified. In the past, certain assumptions are made to obtain the equivalent voltage E and the equivalent inductive reactance XThe equation of (c).
Assume that 1: when a serious voltage drop fault occurs, the inverter is rapidly switched to a low voltage ride through mode, the d-axis reference current is switched to 0, and the q-axis reference current is jointly determined by equation (4) and equation (5);
assume 2: on the premise of hypothesis 1, ignoring the dynamic time scale of the current inner loop, enabling the d-axis current and the q-axis current of the filter inductor to be approximately equal to the reference values, and rapidly converging the d-axis current of the filter inductor and the equivalent inductor at the network side to 0 (a large amount of simulation finds that the simulation result conforms to hypothesis 2);
assume that 3: because the filter capacitor is relatively small, the d-axis current and the q-axis current on the filter inductor are approximately equal to the d-axis current and the q-axis current on the equivalent inductor on the network side in a dynamic state.
Under the quasi-steady state premise, the network side line has an equality relation:
Figure BDA0001475896060000071
wherein, IdoAnd IqoD-axis current and q-axis current flowing through the network side respectively; xEquivalent inductive reactance of a network side; edAnd EqThe components of the equivalent voltage on the network side on the d axis and the q axis are respectively.
Based on assumptions 1 and 3, equation (6) is reduced to:
Vtd=Vt=E-XIq(7)
the above equation (7) represents the equivalent voltage E on the network side and the equivalent reactance X on the lineApproximate equation relationship of (c).
The method adopts a recursive least square method to identify the equivalent voltage E and the line equivalent reactance XThe algorithm only needs to collect the d-axis component V of the local information inverter terminal voltagetdAnd a filter inductor q-axis current component Iq
In a specific implementation, the initial values are set as: theta (0) ═ 01]TP (0) ═ diag { 100100 }, and the sampling period is set to 0.005 s. When a serious voltage drop fault occurs, triggering identification, and when a parameter vector theta (t) to be solved meets max { theta (t) -theta (t-1) }<1e-3Then, the output θ (t) is the recognition result. The specific identification step is shown in FIG. 3.
Specifically, an injected active current amplitude reference value I 'is taken'drefComprises the following steps:
I′dref=0.8E/X(8)
injecting d-axis current amplitude reference value I'drefAs the input of the discrete type active disturbance rejection controller (5), the output of the discrete type active disturbance rejection controller is the reference value I of the injection current of the d axis of the inverterdref
3) And phase-locked loops, current inner loops and voltage feedforward coefficients are optimized. The phase-locked loop parameter self-adaptive adjustment is carried out by adopting the following formula:
Figure BDA0001475896060000072
secondly, optimizing current inner loop parameters: selecting the current inner ring proportion parameter as k p_acc1 and an integration parameter ki_acc=15。
And finally, optimizing the parameters of a voltage feedforward link: reducing voltage feedforward loop parameter afAnd the small interference stability of the system is improved and is set to be 0.002.
The specific embodiment of the invention is as follows:
to verify the validity of the proposed control strategy, the system shown in fig. 1 was simulated in a MATLAB/Simulink environment. The normal control mode of the inverter is an active/alternating voltage control mode, and the system stably runs at P before a faulte0.6pu and VtWhen t is 3s, a far-end voltage drop fault occurs. The main parameters are detailed in table 3.
FIG. 4 shows the line impedance XAnd when the gain coefficient is equal to 4 and the voltage drop degree is equal to 0.2pu, the voltage waveform response curve of the inverter terminal is obtained. It can be seen from fig. 4 that the voltage at the inverter terminal oscillates up and down around 0.9pu, which causes the inverter control mode to switch back and forth between the pre-fault control mode and the typical low voltage control mode, and the inverter is unstable.
FIG. 5 shows an inverter with the low voltage ride through control method of the present invention, in line impedance XWhen the voltage drop degree is 0.2pu, the inverter terminal voltage and the output active power waveform response curve are obtained. When t is equal to 10.08s, the recursive least square method converges, and the obtained E is approximately equal to 0.17pu and X is approximately equal to 0.67pu are identified,calculating to obtain I'drefAnd when the output voltage is approximately equal to 0.20pu, the d-axis current reference value of the inverter is triggered to be switched to the output of the discrete active disturbance rejection controller. As can be seen from a review of fig. 5, during a fault, the inverter terminal voltage returns to the specified value of 0.9pu, and the inverter injects 0.18pu of active power into the grid, illustrating the effectiveness of the proposed control method.
The inverter low voltage ride through control method for the severe voltage fault at the far end of the weak grid according to the present invention is described in detail above, and the principle and the implementation manner of the present invention are illustrated herein by using specific examples, and the above description of the embodiments is only used for explaining the method and the core idea of the present invention, but not limiting the present invention, and any modifications and changes made to the present invention within the spirit of the present invention and the scope of the claims fall within the scope of the present invention.

Claims (5)

1. A low voltage ride through control method of an inverter aiming at a remote severe voltage fault of a weak network is characterized by comprising the following steps: the method comprises the following steps: when a serious voltage fault occurs at the far end of the weak network, the active current in the inverter is controlled to a target value IdrefAnd a reactive current control target amount IqrefSwitching to zero, and designing the control target quantity I of the active current of the inverterdrefAnd a reactive current control target amount IqrefInputting, performing transient transition, optimizing phase-locked loop, current inner loop and voltage feedforward parameters, and improving the stability and dynamic control performance of the inverter during low voltage ride through;
the design inverter active current control target quantity IdrefAnd a reactive current control target amount IqrefInputting, and performing transient transition, specifically:
firstly, obtaining a reactive current amplitude reference value I 'by utilizing integral control'qrefAnd simultaneously identifying and obtaining the equivalent voltage E and the equivalent impedance X of the alternating current power grid by using a recursive least square methodAnd calculating to obtain an active current amplitude reference value I'dref
Then, adopting a discrete active disturbance rejection controller to carry out reactive current amplitude reference value I'qrefAnd active currentAmplitude reference value I'drefProcessing to obtain active current control target quantity I for input inverterdrefAnd a reactive current control target amount Iqref
2. The inverter low voltage ride through control method for the weak grid remote severe voltage fault according to claim 1, characterized in that: obtaining a reactive current amplitude reference value I 'by utilizing integral control'qrefSpecifically, the following formula is adopted:
I′qref=∫ki(Vt-Vtref)dt
wherein k isiIs an integral coefficient, I'qrefInjecting a reactive current amplitude reference value, V, for the invertertTo the inverter terminal voltage, VtrefTo refer to the terminal voltage, t represents time.
3. The inverter low voltage ride through control method for the weak grid remote severe voltage fault according to claim 1, characterized in that: the method for identifying and obtaining the equivalent voltage E and the equivalent impedance X of the alternating current power grid by using the recursive least square methodAnd calculating to obtain an active current amplitude reference value I'drefThe following method is specifically adopted:
1) establishing equivalent voltage E and equivalent impedance X of alternating current power gridThe equality relationship between:
Vtd=Vt=E-XIq
wherein, VtdIs d-axis voltage component of inverter terminal voltage, E is equivalent voltage of AC network, XFor equivalent inductive reactance of the AC mains, IqIs the q-axis current component of the filter inductor;
2) calculating a parameter vector theta (t) to be solved at the t moment by adopting the following formula:
Figure FDA0002386114620000021
in the formula, θ (t) is the parameter vector to be obtained at time t, and θ (t) is [ E X ]]T(ii) a Theta (t-1) is a parameter vector at the t-1 moment; y (t) is an output vector at the time t, and y (t) is equal to the voltage component V of the inverter terminal d axis at the time ttdI.e. y (t) ═ Vtd(t),Vtd(t) V at time ttd
Figure FDA0002386114620000022
For the measurement vector at the time t,
Figure FDA0002386114620000023
Iq(t) represents the q-axis current component of the filter inductor at time t, Id(t) represents the d-axis current component of the filter inductor at time t, Id(t-1) represents a d-axis current component of the filter inductor at the time of t-1; p (t) is an inverse matrix of the covariance at time t; p (t-1) is an inverse matrix of the covariance at the time t-1;
3) if the parameter vector theta (t) to be solved does not satisfy max (theta (t) -theta (t-1) }<1e-3Repeating the step 2) to perform recursive calculation;
if the parameter vector theta (t) to be solved meets max (theta (t) -theta (t-1) }<1e-3Outputting a parameter vector theta (t) to be solved as an identification result, and obtaining the equivalent voltage E of the alternating current power grid and the equivalent inductive reactance X of the alternating current power grid in the identification result
4) Calculating an active current amplitude reference value I 'by adopting the following formula'dref
I′dref=0.8E/X
4. The inverter low voltage ride through control method for the weak grid remote severe voltage fault according to claim 1, characterized in that: the method adopts a discrete active disturbance rejection controller to carry out reactive current amplitude reference value I'qrefAnd an active current amplitude reference value I'drefProcessing to obtain active current control target quantity I for input inverterdrefAnd a reactive current control target amount IqrefThe following method is specifically adopted:
first, a discrete type active disturbance rejection controller of the following formula is established:
Figure FDA0002386114620000024
wherein v is1(t) is the output of the discrete active disturbance rejection controller, v2(t) is v1(t) the derivative of (t), h represents the sampling step, t represents the t-th time interval with h, and r is the amplitude of the amplitude limiter; r is0And h0Are respectively a controller fhan (v)1(t)-v(t),v2(t),r0,h0) Internal gain parameters and step parameters, v (t) is the output of the discrete active disturbance rejection controller; fhan (v)1(t)-v(t),v2(t),r0,h0) Representing the steepest control synthesis function;
then, the active current amplitude is referenced to a value I'drefThe output processed by the discrete type active disturbance rejection controller is used as the input v (t) of the discrete type active disturbance rejection controller as the active current control target quantity Idref(ii) a Reference value I 'of reactive current amplitude'qrefAs an input v ' (t) of another discrete type active disturbance rejection controller, an output v ' processed by the discrete type active disturbance rejection controller '1(t) as a control target amount I of reactive current injected into the inverterqref
5. The inverter low voltage ride through control method for the weak grid remote severe voltage fault according to claim 1, characterized in that: the phase-locked loop, the current inner loop and the voltage feedforward parameter comprise phase-locked loop integral coefficient ki_pllAnd the proportionality coefficient kp_pllIntegral coefficient of inner loop of current ki_accAnd the proportionality coefficient kp_accVoltage feedforward coefficient afSpecifically, the following method is adopted for optimization:
a) self-adaptive optimization phase-locked loop parameters: using inverter terminal voltage amplitude signal VtThe phase-locked loop parameters are optimized in real time by adopting the following formula:
Figure FDA0002386114620000031
in the formula: i VtI is the absolute value of terminal voltage amplitude, kp_pll、ki_pllAre respectively a phase-locked loop proportional coefficient and an integral coefficient k 'before optimization'p_pll、k′i_pllRespectively obtaining an optimized phase-locked loop proportional coefficient and an optimized integral coefficient;
b) optimizing current inner loop parameters: adjusting the current inner loop proportionality coefficient kp_ccAnd integral coefficient ki_accThe current inner loop frequency band is within the range of 300 Hz-350 Hz;
c) optimizing voltage feedforward link parameters: reducing voltage feedforward loop parameter afTo 0.002-0.1.
CN201711164118.8A 2017-11-21 2017-11-21 Inverter low-voltage ride-through control method for weak network far-end severe voltage fault Active CN107732973B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711164118.8A CN107732973B (en) 2017-11-21 2017-11-21 Inverter low-voltage ride-through control method for weak network far-end severe voltage fault

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711164118.8A CN107732973B (en) 2017-11-21 2017-11-21 Inverter low-voltage ride-through control method for weak network far-end severe voltage fault

Publications (2)

Publication Number Publication Date
CN107732973A CN107732973A (en) 2018-02-23
CN107732973B true CN107732973B (en) 2020-05-19

Family

ID=61217764

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711164118.8A Active CN107732973B (en) 2017-11-21 2017-11-21 Inverter low-voltage ride-through control method for weak network far-end severe voltage fault

Country Status (1)

Country Link
CN (1) CN107732973B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110417044B (en) * 2018-04-27 2022-11-22 哈尔滨工业大学 Coordination control method based on permanent magnet synchronous wind power system low voltage ride through
CN111181428B (en) * 2020-01-15 2021-05-14 燕山大学 Zero dynamic direct current output voltage control method and system of current source converter
CN111969647B (en) * 2020-07-24 2022-08-02 南方电网科学研究院有限责任公司 Converter transient instability stabilization control method and device based on state resetting
CN114172212B (en) * 2021-08-20 2023-08-18 华北电力大学(保定) Method for improving transient active power output of photovoltaic unit during low voltage ride through
CN117578536A (en) * 2023-10-19 2024-02-20 上海勘测设计研究院有限公司 Network-structured energy storage control method and system for weak alternating current system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8120932B2 (en) * 2008-07-01 2012-02-21 American Superconductor Corporation Low voltage ride through
CN104868497B (en) * 2015-06-01 2017-07-11 华中科技大学 A kind of control method and system of the double-fed blower fan low voltage crossing without flux observation
CN107147141B (en) * 2017-04-20 2021-01-26 北京金风科创风电设备有限公司 Inverter control method and device of wind generating set

Also Published As

Publication number Publication date
CN107732973A (en) 2018-02-23

Similar Documents

Publication Publication Date Title
CN107732973B (en) Inverter low-voltage ride-through control method for weak network far-end severe voltage fault
CN102157956B (en) Virtual-impedance-based inverter parallel running method
CN105186554B (en) The virtual synchronous generator method for becoming excellent certainly with rotary inertia and damping
Huang et al. A double-PLLs-based impedance reshaping method for extending stability range of grid-following inverter under weak grid
Çelik et al. Voltage support control strategy of grid‐connected inverter system under unbalanced grid faults to meet fault ride through requirements
CN107134936A (en) A kind of inverter active damping control method based on overall-finished housing
CN111130136A (en) Subsynchronous oscillation suppression method based on additional virtual impedance control
CN105356783A (en) Enhanced current-limiting control method aimed at drop-controlled inverter
CN105356781A (en) Control method for inhibiting offset of transient virtual power angle curve of drop-controlled inverter
Alsakati et al. Transient stability enhancement of grid integrated wind energy using particle swarm optimization based multi-band PSS4C
Shair et al. A grid-side multi-modal adaptive damping control of super-/sub-synchronous oscillations in type-4 wind farms connected to weak AC grid
CN107887902B (en) Inverter stability analysis method and system during remote severe voltage drop in weak network
CN111799812B (en) Reactive voltage sensitivity-based reactive coordination control method for offshore wind farm
CN107134796B (en) Improved active-disturbance-rejection-based smooth fire bundling subsynchronous oscillation suppression method
CN116365584A (en) Inverter control mode switching method in distribution network system with multiple inverter access
CN115296341A (en) Power electronic transformer feed network self-adaptive stability controller based on reinforcement learning
CN115102149A (en) Overcurrent suppression system and method for network type converter
Anand et al. Load frequency control of interconnected hydro-hydro system with fuzzy logic controller
CN108110775A (en) A kind of transformer reactive compensation control method based on centralized photovoltaic DC-to-AC converter
CN114006387A (en) Adaptive frequency subsynchronous oscillation suppression method and system based on multi-branch impedance
CN114069697A (en) Method for controlling inverter grid connection based on virtual synchronous generator principle
CN110224415B (en) Self-adaptive error-free frequency modulation control method for micro-grid virtual synchronous machine
CN108462209B (en) Frequency-voltage integrated robust optimization control method based on virtual synchronous generator
CN114123837B (en) High-frequency oscillation suppression method and device for parallel compensation of three-phase four-bridge arm inverter under power grid
CN114400714B (en) Wind power plant voltage hierarchical coordination optimization control method and system

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant