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Control and Design of Microgrid Components - Power Systems ...

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case is when the unit controlling P is the nearest to the utility. The last case is when the two units<br />

are in two separate feeders, Figure 3.24(b). The isl<strong>and</strong> condition is that grid power is zero, which<br />

means that the overall flow in the feeder(s) converging to the utility must be zero. This statement<br />

translates on Figure 3.30 with the condition that F1=0 in isl<strong>and</strong>, since that is the only one feeder<br />

connecting to the grid. This implies that for the unit configuration shown in Figure 3.30, in isl<strong>and</strong><br />

mode the operating point is at frequency ω<br />

1<br />

, lower than the system frequency only because the<br />

flow Fo1 is positive (importing power during grid connection). A negative value for Fo1 would<br />

have generated an intersection with the axis F=0 at a frequency higher than nominal.<br />

Utility<br />

System<br />

F<br />

1<br />

P<br />

1<br />

F<br />

2<br />

L P<br />

2<br />

1<br />

L<br />

2<br />

Unit 1<br />

Regulating<br />

Flow F1<br />

Unit 2<br />

Regulating<br />

Output P2<br />

Figure 3.30 Mixed System on a Single Feeder, with Flow <strong>Control</strong> Near the Utility.<br />

Values <strong>of</strong> output power could exceed limits for the same reasons separately seen in the previous<br />

sections: load change during isl<strong>and</strong> <strong>and</strong> grid, wrong setpoint choice, transfer to isl<strong>and</strong>. The<br />

characteristics <strong>of</strong> Figure 3.29 will need to include features that will enforce limits during steady<br />

state.<br />

The value <strong>of</strong> P at the frequency ω<br />

1<br />

in Figure 3.29 is the amount <strong>of</strong> power generated by the unit<br />

that controls output power. Figure 3.15 with fixed slope, represents the limits for the output<br />

power in the mixed system: this is a rigid characteristic (i.e. does not translate on the P-ω plane).<br />

In Figure 3.15 the constant value used for the slope guaranteed that frequency is within limits as<br />

long as power is held within its own limits.<br />

The unit controlling feeder flow, F, needs to enforce output power limits as it was described on<br />

Figure 3.27. Only a window (Pmax wide) <strong>of</strong> the slanted slope is taken. The location <strong>of</strong> this<br />

window [Fmin, Fmax] varies because it depends on the value <strong>of</strong> the loading condition, as shown<br />

in Eq. 3.10. The overall loading conditions are determined by the loads <strong>and</strong> the generations<br />

behind the unit. In Figure 3.30 the total loading condition (Lt) <strong>of</strong> the first unit (Lt1) includes also<br />

the other load (L2) <strong>and</strong> second unit power output (P2) as a negative contribution to the overall<br />

loading. From Figure 3.30 it is possible to write:<br />

F1 = Lt1-P1<br />

Lt1=L1+L2-P2<br />

This is to show that the physical location <strong>of</strong> the window that represents the limits on the feeder<br />

flow may depend not only on the values <strong>of</strong> the loads, but also on the instantaneous amounts <strong>of</strong><br />

power output <strong>of</strong> other units. The point is that no matter where the sliding window is located, the<br />

48

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