Power System Stabilizers and Discontinuous Excitation Control Transfer Functions (2016)

 

As indicated, each of the power system stabilizer models and discontinuous excitation control models have a unique transfer function. The schematic diagram of each is given below.

For more details, see IEEE Standard 421.5-2016.

Single Input Power System Stabilizer (PSS1A)

 

 

Where,

 

A1, A2  =

Filter constants

KS  =

PSS gain [pu]

T1  =

First Lead time constant [s]

T2  =

First Lag time constant [s]

T4  =

Second Lag time constant [s]

T3  =

Second Lead time constant [s]

T5  =

Washout time constant [s]

T6  =

Transducer time constant [s]

VRMAX, VRMIN  =

Maximum and minimum regulator outputs [pu]

VS1  =

Input

VST  =

Output [pu]

VSTMAX, VSTMIN  =

PSS output maximum and minimum limits [pu]

 

IEEE Power System Stabilizer Type PSS2C

PSS2C is an extended version of PSS2A from IEEE Standard 421.5-1992 and PSS2B from the IEEE Standard 421.5-2005. The PSS2C model shown in the figure below can be used to represent a variety of dual-input stabilizers, which normally use combinations of power and speed (or frequency or compensated frequency) to derive the stabilizing signal. Unlike PSS2B, it allows the representation of the PSS output logic associated with the generator active power output PT, i.e., the PSS output depends on the generator active power output as compared to the thresholds PPSSon and PPSSoff. These threshold values are used to define a hysteresis.
 

 

 

The washout block should be bypassed if the associated time constant is set to zero:

 

IF TW4=0 THEN
  y=u1
ELSE
  y=u2
ENDIF


The PSS output logic uses user-selected parameters PPSSon and PPSSoff. It also uses signal VPSS, shown in the block diagram, and the generator electrical power output PT. The output logic implements the following hysteresis to define the output signal VST:
 


As PSS2C is an extended version of PSS2A as well as PSS2B:

  1. Any PSS represented by the PSS2A model could be represented by the PSS2C model, with the time constants T10 to T13 set equal to each other, in order to bypass the third and fourth lead-lag blocks in the PSS2C model, and the threshold values for the output logic PPSSon and PPSSoff set equal to zero.
  2. Any PSS represented by the PSS2B model could be represented by the PSS2C model, with the time constants T12 and T13 set equal to each other and the threshold values for the output logic PPSSon and PPSSoff set equal to zero.

The tables below give the sample data for PSS2C for some specific excitation system models:

 

For the AC6C & ST1C model:

 

Description Symbol Type Value Units

PSS Gain

KS1 A 20 pu

PSS Gain

KS2 E/A a pu

PSS Gain

KS3 E 1 pu

PSS Transducer Time Constant

T6 E 0.0 s

PSS Transducer Time Constantb

T7 A 10 s

PSS Washout Time Constant

Tw1 A 10 s

PSS Washout Time Constant

Tw2 A 10 s

PSS Washout Time Constant

Tw3 A 10 s

PSS Washout Time Constant

Tw4 A c s

PSS Transducer Time Constant

T8 A 0.3 s

PSS Washout Time Constant

T9 A 0.15 s

PSS Transducer Time Constant Exponent

M A 2  

PSS Transducer Time Constant Exponent

N A 4  

PSS Numerator (lead) Compensating Time Constant (first block)

T1 A 0.16 s

PSS Denominator (lag) Compensating Time Constant (first block)

T2 A 0.02 s

PSS Numerator (lead) Compensating Time Constant (second block)

T3 A 0.16 s

PSS Denominator (lag) Compensating Time Constant (second block)

T4 A 0.02 s

PSS Numerator (lead) Compensating Time Constant (third block)

T10 A d s

PSS Denominator (lag) Compensating Time Constant (third block)

T11 A d s

PSS Numerator (lead) Compensating Time Constant (fourth block)

T12 A e s

PSS Denominator (lag) Compensating Time Constant (fourth block)

T13 A e s

Maximum PSS Output

VSTmax A 0.20 pu

Minimum PSS Output

VSTmin A -0.066 pu

Input Signal # 1 Maximum Limit

VSI1max A 2 pu

Input Signal # 1 Minimum Limit

VSI1min A -2 pu

Input Signal # 2 Maximum Limit

VSI2max A 2 pu

Input Signal # 2 Minimum Limit

VSI2min A -2 pu

Generator MW Threshold for PSS Activation

PPSSon A 0 pu

Generator MW Threshold for PSS De-activation

PPSSoff A 0 pu

 

Notes: 

 

PSS settings depend not only on the excitation system model and parameters, but also on the generator model. These PSS parameters might not work properly for different generator models, even if the excitation system model remains the same.

  1. The gain KS2 should be calculated as T7/(2H), where H is the total shaft inertia of all mechanically connected rotating components of the unit (MW-s/MVA).
  2. The time constant T7 should be equal to Tw2.
  3. The washout block with time constant Tw4 should be bypassed. Set Tw4 as necessary to bypass this block, based on the documentation of the software being used and the description in IEEE Standard 421.5-2016 (Section E.7).
  4. The third lead-lag block is not used in this example. Set T10 = T11 or follow the instructions in the documentation of the software being used.
  5. The fourth lead-lag block is not used in this example. Set T12 = T13 or follow the instructions in the documentation of the software being used.

For the AC7C model:

 

Description Symbol Type Value Units

PSS Gain

KS1 A 5 pu

PSS Gain

KS2 E/A a pu

PSS Gain

KS3 E 1 pu

PSS Transducer Time Constant

T6 E 0.0 s

PSS Transducer Time Constantb

T7 A 10 s

PSS Washout Time Constant

Tw1 A 10 s

PSS Washout Time Constant

Tw2 A 10 s

PSS Washout Time Constant

Tw3 A 10 s

PSS Washout Time Constant

Tw4 A c s

PSS Transducer Time Constant

T8 A 0.5 s

PSS Washout Time Constant

T9 A 0.1 s

PSS Transducer Time Constant Exponent

M A 5  

PSS Transducer Time Constant Exponent

N A 1  

PSS Numerator (lead) Compensating Time Constant (first block)

T1 A 0.16 s

PSS Denominator (lag) Compensating Time Constant (first block)

T2 A 0.04 s

PSS Numerator (lead) Compensating Time Constant (second block)

T3 A 0.16 s

PSS Denominator (lag) Compensating Time Constant (second block)

T4 A 0.04 s

PSS Numerator (lead) Compensating Time Constant (third block)

T10 A 0.18 s

PSS Denominator (lag) Compensating Time Constant (third block)

T11 A 0.03 s

PSS Numerator (lead) Compensating Time Constant (fourth block)

T12 A d s

PSS Denominator (lag) Compensating Time Constant (fourth block)

T13 A d s

Maximum PSS Output

VSTmax A 0.10 pu

Minimum PSS Output

VSTmin A -0.10 pu

Input Signal # 1 Maximum Limit

VSI1max A 2 pu

Input Signal # 1 Minimum Limit

VSI1min A -2 pu

Input Signal # 2 Maximum Limit

VSI2max A 2 pu

Input Signal # 2 Minimum Limit

VSI2min A -2 pu

Generator MW Threshold for PSS Activation

PPSSon A 0 pu

Generator MW Threshold for PSS De-activation

PPSSoff A 0 pu

 

Notes: 

 

PSS settings depend not only on the excitation system model and parameters, but also on the generator model. These PSS parameters might not work properly for different generator models, even if the excitation system model remains the same.

  1. The gain KS2 should be calculated as T7/(2H), where H is the inertia constant of the generator (MW-s/MVA).
  2. The time constant T7 should be equal to Tw2.
  3. The washout block with time constant Tw4 should be bypassed. Set Tw4 as necessary to bypass this block, based on the documentation of the software being used and the description in IEEE Standard 421.5-2016 (Section E.7).
  4. The fourth lead-lag block is not used in this example. Set T12 = T13 or follow the instructions in the documentation of the software being used.

IEEE Power System Stabilizer Type PSS3C

PSS3C is an extended version of PSS3B from the IEEE Standard 421.5-2005. The PSS3C model shown in the figure below has dual inputs, usually generator electrical power output (VSI1 = PT) and rotor angular speed deviation (VSI2  = Δω). The signals are used to derive an equivalent mechanical power signal. By properly combining this signal with electrical power a signal proportional to accelerating power is produced.

 

 

 

The PSS output logic uses user-selected parameters PPSSon and PPSSoff. It also uses signal VPSS, shown in the block diagram, and the generator electrical power output PT. The output logic implements the following hysteresis to define the output signal VST:

 


As PSS3C is an extended version of PSS3B, any PSS represented by the PSS3B model could also be represented by the PSS3C model, by setting the PSS3C parameters associated with the PSS output logic (PPSSon and PPSSoff) to zero.


The table below gives the sample data for PSS3C:

 

Description Symbol Type Value Units

PSS Gain (input channel 1)

KS1 A 1 pu

PSS Gain (input channel 2)

KS2 A 0 pu

PSS Transducer Time Constant (input channel 1)

T1 E/A 0.02 s

PSS Transducer Time Constant (input channel 2)

T2 E/A 1.5 s

PSS Washout Time Constant (input channel 1)

Tw1 A 1.5 s

PSS Washout Time Constant (input channel 2)

Tw2 A 1.5 s

PSS Washout Time Constant (combined channels)

Tw3 A 0 s

PSS Numerator Coefficient (first block)

A1 A 0  

PSS Numerator Coefficient (first block)

A2 A 0  

PSS Denominator Coefficient (first block)

A3 A 0  

PSS Denominator Coefficient (first block)

A4 A 0  

PSS Numerator Coefficient (second block)

A5 A 0  

PSS Numerator Coefficient (second block)

A6 A 0  

PSS Denominator Coefficient (second block)

A7 A 0  

PSS Denominator Coefficient (second block)

A8 A 0  

PSS Numerator (lead) Compensating Time Constant (fourth block)

T12 A d s

PSS Denominator (lag) Compensating Time Constant (fourth block)

T13 A d s

Maximum PSS Output

VSTmax A 0.10 pu

Minimum PSS Output

VSTmin A -0.10 pu

Generator MW Threshold for PSS Activation

PPSSon A 0 pu

Generator MW Threshold for PSS De-activation

PPSSoff A 0 pu

 

IEEE Power System Stabilizer Type PSS4C

PSS4C is an extended version of PSS4B from the IEEE Standard 421.5-2005. The PSS4C model’s structure is based on multiple working frequency bands as shown in the figure below. Four separate bands respectively dedicated to the very low, low, intermediate, and high-frequency modes of oscillations are used in this delta-omega (speed input) PSS.

 

 

The PSS4C measures the rotor speed deviation in two different ways. The input signal Δω(L-I) feeds the very low, low, and intermediate bands while the input signal ΔωH is dedicated to the high-frequency band. The equivalent model of these two-speed transducers is shown in the figure below. Tuneable notch filters Ni(s), can be used for turbo-generators with well-tuned notch filters attenuating PSS gain at torsional mode  frequencies, generally above 10 Hz, as shown below:

 

 

Where,

 

ωni is the filter frequency
Bωi is the filter 3 dB bandwidth  
 

As PSS4C is an extended version of PSS4B, any PSS represented by the PSS4B model could also be represented by the PSS4C model, by setting the PSS4C parameters in order to ignore the very low-frequency band. This is easily done by setting the gain KVL equal to zero. 


The table below gives the sample data for PSS4C:
 

Description Symbol Type Value Units

Very Low Band Gain

KVL A 0.5 pu

Very Low Band Differential Filter Gain

KVL1 A 66 pu

Very Low Band First Lead-lag Block Coefficient

KVL11 A 1 pu

Very Low Band Numerator Time Constant (first lead-lag block)

TVL1 A 12.1 s

Very Low Band Denominator Time Constant (first lead-lag block)

TVL2 A 14.5 s

Very Low Band Numerator Time Constant (second lead-lag block)

TVL3 A 0 s

Very Low Band Denominator Time Constant (second lead-lag block)

TVL4 A 0 s

Very Low Band Numerator Time Constant (third lead-lag block)

TVL5 A 0 s

Very Low Band Denominator Time Constant (third lead-lag block)

TVL6 A 0 s

Very Low Band Differential Filter Gain

KVL2 A 66 pu

Very Low Band First Lead-lag Block Coefficient

KVL17 A 1 pu

Very Low Band Numerator Time Constant (first lead-lag block)

TVL7 A 14.5 s

Very Low Band Denominator Time Constant (first lead-lag block)

TVL8 A 17.4 s

Very Low Band Numerator Time Constant (second lead-lag block)

TVL9 A 0 s

Very Low Band Denominator Time Constant (second lead-lag block)

TVL10 A 0 s

Very Low Band Numerator Time Constant (third lead-lag block)

TVL11 A 0 s

Very Low Band Denominator Time Constant (third lead-lag block)

TVL12 A 0 s

Very Low Band Upper Limit

VVLmax A 0.01 pu

Very Low Band Lower Limit

VVLmin A -0.01 pu

Low Band Gain

KL A 3 pu

Low Band Differential Filter Gain

KL1 A 66 pu

Low Band First Lead-lag Block Coefficient

KL11 A 1 pu

Low Band Numerator Time Constant (first lead-lag block)

TL1 A 1.73 s

Low Band Denominator Time Constant (first lead-lag block)

TL2 A 2.075 s

Low Band Numerator Time Constant (second lead-lag block)

TL3 A 0 s

Low Band Denominator Time Constant (second lead-lag block)

TL4 A 0 s

Low Band Numerator Time Constant (third lead-lag block)

TL5 A 0 s

Low Band Denominator Time Constant (third lead-lag block)

TL6 A 0 s

Low Band Differential Filter Gain

KL2 A 66 pu

Low Band First Lead-lag Block Coefficient

KL17 A 1 pu

Low Band Numerator Time Constant (first lead-lag block)

TL7 A 2.075 s

Low Band Denominator Time Constant (first lead-lag block)

TL8 A 2.491 s

Low Band Numerator Time Constant (second lead-lag block)

TL9 A 0 s

Low Band Denominator Time Constant (second lead-lag block)

TL10 A 0 s

Low Band Numerator Time Constant (third lead-lag block)

TL11 A 0 s

Low Band Denominator Time Constant (third lead-lag block)

TL12 A 0 s

Low Band Upper Limit

VLmax A 0.075 pu

Low Band Lower Limit

VLmin A -0.075 pu

Intermediate Band Gain

KI A 20 pu

Intermediate Band Differential Filter Gain

KI1 A 66 pu

Intermediate Band First Lead-lag Block Coefficient

KI11 A 1 pu

Intermediate Band Numerator Time Constant (first lead-lag block)

TI1 A 0.2018 s

Intermediate Band Denominator Time Constant (first lead-lag block)

TI2 A 0.2421 s

Intermediate Band Numerator Time Constant (second lead-lag block)

TI3 A 0 s

Intermediate Band Denominator Time Constant (second lead-lag block)

TI4 A 0 s

Intermediate Band Numerator Time Constant (third lead-lag block)

TI5 A 0 s

Intermediate Band Denominator Time Constant (third lead-lag block)

TI6 A 0 s

Intermediate Band Differential Filter Gain

KI2 A 66 pu

Intermediate Band First Lead-lag Block Coefficient

KI17 A 1 pu

Intermediate Band Numerator Time Constant (first lead-lag block)

TI7 A 0.2421 s

Intermediate Band Denominator Time Constant (first lead-lag block)

TI8 A 0.2906 s

Intermediate Band Numerator Time Constant (second lead-lag block)

TI9 A 0 s

Intermediate Band Denominator Time Constant (second lead-lag block)

TI10 A 0 s

Intermediate Band Numerator Time Constant (third lead-lag block)

TI11 A 0 s

Intermediate Band Denominator Time Constant (third lead-lag block)

TI12 A 0 s

Intermediate Band Upper Limit

VImax A 0.6 pu

Intermediate Band Lower Limit

VImin A -0.6 pu

High Band Gain

KH A 80 pu

High Band Differential Filter Gain

KH1 A 66 pu

High Band First Lead-lag Block Coefficient

KH11 A 1 pu

High Band Numerator Time Constant (first lead-lag block)

TH1 A 0.01345 s

High Band Denominator Time Constant (first lead-lag block)

TH2 A 0.01614 s

High Band Numerator Time Constant (second lead-lag block)

TH3 A 0 s

High Band Denominator Time Constant (second lead-lag block)

TH4 A 0 s

High Band Numerator Time Constant (third lead-lag block)

TH5 A 0 s

High Band Denominator Time Constant (third lead-lag block)

TH6 A 0 s

High Band Differential Filter Gain

KH2 A 66 pu

High Band First Lead-lag Block Coefficient

KH17 A 1 pu

High Band Numerator Time Constant (first lead-lag block)

TH7 A 0.01614 s

High Band Denominator Time Constant (first lead-lag block)

TH8 A 0.01937 s

High Band Numerator Time Constant (second lead-lag block)

TH9 A 0 s

High Band Denominator Time Constant (second lead-lag block)

TH10 A 0 s

High Band Numerator Time Constant (third lead-lag block)

TH11 A 0 s

High Band Denominator Time Constant (third lead-lag block)

TH12 A 0 s

High Band Upper Limit

VHmax A 0.60 pu

High Band Lower Limit

VHmin A -0.60 pu

Maximum PSS Output

VSTmax A 0.15 pu

Minimum PSS Output

VSTmin A -0.15 pu

 

NOTE 1: PSS settings depend not only on the excitation system model and parameters, but also on the generator model. These PSS parameters might not work properly for different generator models, even if the excitation system model remains the same.


NOTE 2: Refer to the figure above regarding the input signals for the PSS4C model. This is a dual-input model using rotor speed and generator electrical power output as inputs.

 

IEEE Power System Stabilizer Type PSS5C

PSS5C represents a simplifying model of the PSS4C. Like the PSS4C, the PSS5C model represents a structure based on multiple working frequency bands as shown in the figure below, but this model uses only four gains and four central frequencies, and the ten limits associated for a total of eighteen parameters. The principal difference is the transducer for which only one input is used as shown in the figure below. Compared with the PSS4C model, this model is easier for tuning studies, but it has a limitation as it cannot represent the rate of change of electrical power (MW/minute) which affects the output of the on-site stabilizer. For studying and stability software where f ≤ 3 Hz, the notch filters could be omitted.

 

 

 

The table below gives the sample data for PSS5C:

 

Description Symbol Type Value Units

Very Low Band Gain

KVL A 0.5 pu

Very Low Band Central Frequency

KVL1 A 0.01 Hz

Very Low Band Upper Limit

VVLmax A 0.01 pu

Very Low Band Lower Limit

VVLmin A -0.01 pu

Low Band Gain

KL A 3 pu

Low Band Central Frequency

KL1 A 0.07 Hz

Low Band Upper Limit

VLmax A 0.075 pu

Low Band Lower Limit

VLmin A -0.075 pu

Intermediate Band Gain

KI A 20 pu

Intermediate Band Central Frequency

KI1 A 0.6 Hz

Intermediate Band Upper Limit

VImax A 0.60 pu

Intermediate Band Lower Limit

VImin A -0.60 pu

High Band Gain

KH A 80 pu

High Band Central Frequency

KH1 A 9 Hz

High Band Upper Limit

VHmax A 0.60 pu

High Band Lower Limit

VHmin A -0.60 pu
  k1 A 5.736  
  k2 A 6.883  
  k3 A 8.259  

Maximum PSS Output

VSTmax A 0.15 pu

Minimum PSS Output

VSTmin A -0.15 pu

 

NOTE 1: PSS settings depend not only on the excitation system model and parameters, but also on the generator model. These PSS parameters might not work properly for different generator models, even if the excitation system model remains the same.


NOTE 2: Refer to the figure above regarding the input signals for the PSS5C model. This is a single-input model using rotor speed as the input signal.
 

IEEE Power System Stabilizer Type PSS6C

PSS6C shown in the figure below is related to the PSS3C. The PSS6C model also has dual inputs, usually generator electrical power output (VSI1 = PT) and rotor angular speed deviation (VSI2  = Δω). The signals are used to derive an equivalent mechanical power signal. By properly combining this signal with electrical power a signal proportional to accelerating power is produced.

 

 

The PSS output logic uses user-selected parameters PPSSon and PPSSoff. It also uses signal VPSS, shown in the block diagram, and the generator electrical power output PT. The output logic implements the following hysteresis to define the output signal VST:

 

 
It is possible to convert parameters from a PSS3B model into a PSS6C model and vice-versa, but this is not a trivial task, as it might require solving polynomials equations of up to fourth order. For details, see IEEE Standard 421.5-2016.

 

The table below gives the sample data for PSS6C:

 

Description Symbol Type Value Units

PSS Gain (input signal 1)

KS1 A 20 pu

PSS Transducer Time Constant (input signal 1)

T1 E/A 0.01 s

PSS Time Constant (input signal 1)

T3 A 0.4405 s

PSS Gain (input signal 2)

KS2 E/A 1 pu

PSS Washout Time Constant (input signal 2)

Macc A 20.6838 s

PSS Transducer Time Constant (input signal 2)

T2 E/A 0.01 s

PSS Time Constant (input signal 2)

T4 A 0.4405 s

PSS Washout Time Constant

TD A 1.7809 s

PSS Canonical Gain 0

K0 A 1.3322 pu

PSS Canonical Gain 1

K1 A 0.2903 pu

PSS Canonical Gain 2

K2 A 0.7371 pu

PSS Canonical Gain 3

K3 A 0.0813 pu

PSS Canonical Gain 4

K4 A 0 pu

PSS Third Block Gaina

Ki3 A 1 pu

PSS Fourth Block Gainb

Ki4 A 0 pu

PSS Main Block Gain

K5 A 1 pu

PSS Time Constant (first block)

T1 A 0.16 s

PSS Time Constant (second block)

T3 A 0.16 s

PSS Time Constant (third block)

T10 A d s

PSS Time Constant (fourth block)

T12 A e s

Maximum PSS Output

VSTmax A 0.05 pu

Minimum PSS Output

VSTmin A -0.05 pu

Input Signal # 1 Maximum Limit

VST1max A 2 pu

Input Signal # 1 Minimum Limit

VST1min A -2 pu

Input Signal # 2 Maximum Limit

VST2max A 2 pu

Input Signal # 2 Minimum Limit

VST2min A -2 pu

Generator MW Threshold for PSS Activation

PPSSon A 0.21 pu

Generator MW Threshold for PSS De-activation

PPSSoff A 0.19 pu

 

Notes: 

 

PSS settings depend not only on the excitation system model and parameters, but also on the generator model. These PSS parameters might not work properly for different generator models, even if the excitation system model remains the same.

  1. Third block is used in this example, Ki3 = 1.
  2. Fourth block is not used in this example, Ki4 = 0.

IEEE Power System Stabilizer Type PSS7C

The PSS7C model shown in the figure below is a hybrid of the PSS2C and the PSS6C. The PSS7C model has exactly the same structure of the PSS2C from the dual inputs up to the main PSS gain KS1. The phase compensation, however, is provided by a canonical state equation, similar to what is applied in the PSS6C.

 

 

The PSS output logic uses user-selected parameters PPSSon and PPSSoff. It also uses signal VPSS, shown in the block diagram, and the generator electrical power output PT. The output logic implements the following hysteresis to define the output signal VST:

 

 
It is possible to convert the parameters of a PSS2C into the canonical form of the PSS7C. On the other hand, it might not be possible to convert the parameters from the PSS7C back to a PSS2C, as the canonical form might result in complex poles or zeros that cannot be represented by the lead-lag blocks in the PSS2C. For details, see IEEE Standard 421.5-2016.

 

The table below gives the sample data for PSS7C:

 

Description Symbol Type Value Units

PSS Main Gain

KS1 A 50 pu

PSS Gaina

KS2 E/A 0.7052 pu

PSS Gain

KS3 E 1 pu

PSS Transducer Time Constant

T6 E 0 s

PSS Transducer Time Constantb

T7 A 10 s

PSS Washout Time Constant

Tw1 A 10 s

PSS Washout Time Constant

Tw2 A 10 s

PSS Washout Time Constant

Tw3 A 10 s

PSS Washout Time Constant

Tw4 A c s

PSS Transducer Time Constant

T8 A 0.5 s

PSS Washout Time Constant

T9 A 0.1 s

Denominator Exponent for Ramp-track Filter

M A 5  

Overall Exponent for Ramp-track Filter

N A 1  

PSS Canonical Gain 0

K0 A 0.399 pu

PSS Canonical Gain 1

K1 A 1.8462 pu

PSS Canonical Gain 2

K2 A 0.4231 pu

PSS Canonical Gain 3

K3 A 0.2104 pu

PSS Canonical Gain 4

K4 A 0 pu

PSS Third Block Gaind

Ki3 A 1 pu

PSS Fourth Block Gaine

Ki4 A 0 pu

PSS Time Constant (first block)

Ti1 A 0.03 s

PSS Time Constant (second block)

Ti2 A 0.0293 s

PSS Time Constant (third block)

Ti3 A 0.2804 s

PSS Time Constant (fourth block)

Ti4 A 1 s

Maximum PSS Output

VSTmax A 0.05 pu

Minimum PSS Output

VSTmin A -0.05 pu

Input Signal # 1 Maximum Limit

VSI1max A 2 pu

Input Signal # 1 Minimum Limit

VSI1min A -2 pu

Input Signal # 2 Maximum Limit

VSI2max A 2 pu

Input Signal # 2 Minimum Limit

VSI2min A -2 pu

Generator MW Threshold for PSS Activation

PPSSon A 0.21 pu

Generator MW Threshold for PSS De-activation

PPSSoff A 0.10 pu

 

Notes: 

 

PSS settings depend not only on the excitation system model and parameters, but also on the generator model. These PSS parameters might not work properly for different generator models, even if the excitation system model remains the same.

  1. The gain KS2 should be calculated as T7/(2H), where H is the inertia constant of the generator (MW-s/MVA).
  2. The time constant T7 should be equal to Tw2.
  3. The washout block with time constant Tw4 should be bypassed. Set Tw4 as necessary to bypass this block, based on the documentation of the software being used.
  4. Third block is used in this example, Ki3 = 1.
  5. Fourth block is not used in this example, Ki4 = 0.

IEEE Discontinuous Excitation Control Type DEC1A

DEC1A discontinuous excitation control, shown in the figure below, is used to represent a scheme that boosts generator excitation to a level higher than that demanded by the voltage regulator and stabilizer immediately following a system fault. For details, see IEEE Standard 421.5-2016.

 

 

 

IF VT>VTM THEN

  VP=VOmax

ELSEIF  VT<VTN THEN

  VP=0

ELSE

  VP is unchanged (retains previous value)

ENDIF

 

IEEE Discontinuous Excitation Control Type DEC2A

DEC2A discontinuous excitation control is shown in the figure below. This system provides transient excitation boosting via an open loop control as initiated by a trigger signal generated remotely. For details, see IEEE Standard 421.5-2016.

 

 

 

IEEE Discontinuous Excitation Control Type DEC3A

DEC3A discontinuous excitation control is shown in the figure below. In some systems, the PSS output is disconnected from the regulator immediately following a severe fault to prevent the stabilizer from competing with action of voltage regulator during the first swing. This is accomplished in the DEC3A.

 

 

 

 

IF VT>VTmin THEN

  Open switch S1 and keep it open for the given time TDR

ELSE

  Switch S1 is closed, VS=VST

ENDIF