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Induction Motor Load Dynamics: Impact on Voltage Recovery ...

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2<br />

representati<strong>on</strong>. Secti<strong>on</strong> V presents some preliminary results<br />

with an example test system that comprises inducti<strong>on</strong> motor<br />

loads. Finally, secti<strong>on</strong> VI c<strong>on</strong>cludes the paper.<br />

II. PROBLEM STATEMENT<br />

The problem of transient voltage sags during .disturbances<br />

and recovery after the disturbance has been removed is quite<br />

well known. The importance of the problem has been well<br />

identified; its significance is increasing especially in modern<br />

restructured power systems that may frequently operate close<br />

to their limits under heavy loading c<strong>on</strong>diti<strong>on</strong>s. Furthermore,<br />

the increased number of voltage-sensitive loads and the<br />

requirements for improved power system reliability and power<br />

quality are imposing more strict criteria for the voltage<br />

recovery after severe disturbances. It is well known that slow<br />

voltage recovery phenomena have sec<strong>on</strong>dary effects such as<br />

operati<strong>on</strong> of protective relays, electric load disrupti<strong>on</strong>, motor<br />

stalling, etc. Many sensitive loads may have stricter settings of<br />

protective equipment and therefore will trip faster in the<br />

presence of slow voltage recovery resulting in loss of load<br />

with severe ec<strong>on</strong>omic c<strong>on</strong>sequences. A typical situati<strong>on</strong> of<br />

voltage recovery following a disturbance is illustrated in Fig.<br />

1. Note there is a fault during which the voltage collapses to a<br />

certain value. When the fault clears, the voltage recovers<br />

quickly to another level and then slowly will build up to the<br />

normal voltage. The last period of slow recovery is mostly<br />

affected by the load dynamics and especially inducti<strong>on</strong> motor<br />

behavior.<br />

The objective of the paper is to present a method that can<br />

be used to study voltage recovery events after a disturbance.<br />

More specifically the problem is stated as follows: Assume a<br />

power system with dynamic loads, like, for example,<br />

inducti<strong>on</strong> motors. A fault occurs at some place in the system<br />

and it is cleared by the protecti<strong>on</strong> devices after some period of<br />

time. The objective it to study the voltage recovery after the<br />

disturbance has been cleared at the buses where dynamic or<br />

other sensitive loads are c<strong>on</strong>nected and also determine how<br />

these loads affect the recovery process.<br />

This paper proposes a hybrid approach to the study of<br />

voltage recovery that is based <strong>on</strong> static load flow techniques<br />

taking also into account the essential dynamic features of the<br />

load. This approach provides a more realistic tool compared to<br />

traditi<strong>on</strong>al load flow, avoiding however the full scale transient<br />

simulati<strong>on</strong> which requires detailed system and load dynamic<br />

models.<br />

III. SINGLE-PHASE QUADRATIZED POWER FLOW (SPQPF)<br />

WITH INDUCTION MOTOR REPRESENTATION<br />

A. Overview of Single Phase Quadratized Power Flow<br />

The proposed system modeling is based <strong>on</strong> the single phase<br />

quadratized power flow. The idea of this power flow model is<br />

to have a set of power flow equati<strong>on</strong>s of degree no greater<br />

than two, i.e. have a set of linear or quadratic equati<strong>on</strong>s. This<br />

can be achieved without making any sort of approximati<strong>on</strong>s,<br />

so the power system model is an exact model. Since most of<br />

the equati<strong>on</strong>s turn out to be linear and the degree of<br />

n<strong>on</strong>linearity for the n<strong>on</strong>linear equati<strong>on</strong>s is restricted to at most<br />

two, this results in improved c<strong>on</strong>vergence characteristics in<br />

the iterative soluti<strong>on</strong> and therefore improved executi<strong>on</strong> speed<br />

at no expense in the accuracy of the soluti<strong>on</strong>.<br />

<strong>Voltage</strong> (pu)<br />

1.00<br />

0.95<br />

0.90<br />

0.85<br />

0.80<br />

0.75<br />

0.70<br />

0.65<br />

0.60<br />

Fault<br />

Fault Cleared<br />

<str<strong>on</strong>g>Motor</str<strong>on</strong>g>s will trip<br />

if voltage sags<br />

for too l<strong>on</strong>g<br />

-1.00 -0.50 0.00 0.50 1.00 1.50 2.00<br />

Sec<strong>on</strong>ds<br />

Fig. 1. Possible behavior of voltage recovery during and after a disturbance.<br />

The first step in expressing the power flow equati<strong>on</strong>s in<br />

quadratic form is to avoid the trig<strong>on</strong>ometric n<strong>on</strong>linearities.<br />

This can be achieved by utilizing rectangular coordinates<br />

instead of the traditi<strong>on</strong>ally used polar coordinates for<br />

expressing the voltage phasors. Therefore, the system states<br />

are not the voltage magnitudes and angles, but instead the real<br />

and imaginary parts of the voltage phasors. This results in a<br />

set of polynomial equati<strong>on</strong>s. If the degree of n<strong>on</strong>linearity of<br />

these equati<strong>on</strong>s is more than two, then quadratizati<strong>on</strong> of the<br />

equati<strong>on</strong>s can be achieved by introducing additi<strong>on</strong>al state<br />

variables. Note that the quadratizati<strong>on</strong> is performed without<br />

any approximati<strong>on</strong>s, and the resulting quadratic model is an<br />

exact model.<br />

The system modeling is performed <strong>on</strong> the device level, i.e.<br />

a set of quadratic equati<strong>on</strong>s is used to represent the model of<br />

each device. A generalized comp<strong>on</strong>ent model is used,<br />

representing every device, which c<strong>on</strong>sists of the current<br />

equati<strong>on</strong>s of each device, which relate the current through the<br />

device to the states of the device, al<strong>on</strong>g with additi<strong>on</strong>al<br />

internal equati<strong>on</strong>s that model the operati<strong>on</strong> of the device. The<br />

general form of the model, for any comp<strong>on</strong>ent k , is as in (1)<br />

k<br />

i<br />

<br />

Y<br />

0<br />

<br />

k<br />

x<br />

k<br />

x<br />

<br />

x<br />

<br />

<br />

<br />

k T<br />

k T<br />

k k<br />

F x <br />

1<br />

<br />

k k<br />

F x b , (1)<br />

2<br />

<br />

<br />

<br />

k<br />

i is the current through the comp<strong>on</strong>ent,<br />

x k is the<br />

where<br />

vector of the comp<strong>on</strong>ent states and b k the driving vector for<br />

each comp<strong>on</strong>ent. Matrix Y k models the linear part of the<br />

comp<strong>on</strong>ent and matrices F the n<strong>on</strong>linear (quadratic) part.<br />

k<br />

i

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