2.1. Dynamic Model of Power System Frequency
A set of wind turbogenerators is composed of two opposite rotating torques: the mechanical torque of the turbine and the electromagnetic torque of the generator. The motion equation can be expressed as follows:
Equation (1) represents the first-order swing equation, considering the system during steady state
, both sides of the equation can be divided by
simultaneously to obtain the mechanical equations of motion expressed in terms of the active power:
Rocof (Rate of Change of Frequency) represents the rate of system frequency variation. At the instant when a power deficit occurs, the system frequency drops rapidly like an approximately straight line. By taking the derivative of the equation at time
t, the maximum value of the rate of change of system frequency can be obtained:
The frequency characteristic of a power system is related to the real-time active power balance of the system.
Figure 1 shows the typical frequency dynamic curve of a power system after a fault disturbance, and the frequency change process can be divided into inertial response, primary frequency control, secondary frequency control, and tertiary frequency control. Some literature divides the time period before the inertial response into the fast response period.
The frequency stability of a power system may be challenged by major disturbances such as generator tripping, sudden heavy load changes, or system islanding events caused by breaker trips on interconnecting lines. After such disturbances, the system frequency will drop to a minimum point and then enter a new equilibrium point () below the nominal value (i.e., 50 Hz). Several indicators are used to describe the dynamic performance of the system during this process, including the minimum frequency point (), the time to reach the minimum frequency point (), and the rate of frequency change ().
Inertial response takes effect immediately after a power system fault occurs before the governor begins to act. As shown by the yellow dashed line in
Figure 1, the initial drop rate of the system frequency is directly proportional to the system inertia level, and the frequency drops in an approximately radial direction. In low-inertia systems, especially in power systems with a high proportion of renewable energy sources after grid connection, insufficient inertia level may lead to a rapid drop in frequency.
When the time exceeds the dead band of the speed controller, the speed controller begins to act, and the frequency drop rate gradually slows down. The speed controller increases the mechanical power output of the unit, thereby reducing the power deviation and suppressing the frequency drop. When the mechanical power is momentarily equal to the electromagnetic power, the lowest frequency drop appears at time . The primary frequency control is proportional control, and the frequency rise stops at the steady-state value . The duration of this stage is approximately 5 to 25 s.
The second frequency control stage initiates the AGC control to change the output power of the primary motor and slowly eliminate the frequency control deviation in the slow control region. The goal is to restore power balance at the rated frequency, and the duration is about 30 s to 15 min (). Afterward, the third frequency control stage involves the unit’s rescheduling to respond to the next frequency safety incident, with a duration of more than 30 min ().
It should be noted that, if we normalize both sides of the equation using the value of total load demand, then the damping of the load, represented by D, will be a constant that is independent of the load level. Meanwhile, the parameter H will be determined solely by the characteristics of the thermal generator and will not be affected by its installed capacity. In this article, it is assumed that all frequency equations are normalized by load demand.
2.2. Frequency Support Provided by Wind Turbines
Renewable energy is connected to the grid through converters, and its power is decoupled from the grid frequency; therefore, it does not have the inertia and damping characteristics of synchronous generators. With the development of grid-connected inverters and virtual inertia control technology, renewable energy can provide frequency support through control strategies. At this point, the power system with renewable energy includes both Variable Renewable Energy (VRE) and thermal power units to provide equivalent inertia.
Figure 2 presents the power system in northern China, which consists mainly of a combination of thermal generators and wind farms based on grid-connected power electronics. and the frequency response model is changed to:
represents the virtual inertia of the renewable energy system, and represents the adjustment amount of the active power output of the VRE.
The frequency response characteristics of the system usually need to consider the regulating effect of damping, and the change of mechanical power is the co-determination determined by the governor and turbine characteristics.
Figure 3 presents the frequency response model of the aggregated system, whereby the time domain expression of the system after power disturbance
can be calculated:
The frequency security index is represented by the following equation:
where
and
Equation (6) represent the time-domain expression of the lowest point of the system frequency, the rate of frequency change, and the time of the lowest point of frequency drop, which are key indicators representing the frequency change after system disturbance. More details can be found in [
25].
2.3. Modeling and Linearization of Safety Constraints for High Ratio Wind Power Frequency
In this section, due to the complexity of the high-order non-linear function
mapping between the minimum frequency point and the shortage power, when
is fixed, the
function has a monotonic characteristic in a local range of a single parameter, as shown in
Figure 4. However, it is still difficult to handle for establishing a constraint model. Therefore, it is necessary to segment and linearize the function, so that it can be included in the unit dispatch model as a solvable linear programming problem.
This subsection uses the piecewise linearization method to linearize the frequency power mapping function. First, a series of sample points
are generated through equation
, and the generated sample points are divided into K sample subspaces. In order to enable the resulting approximate function to be linearly represented by decision variables, [
] is selected as the variable for the sub-sample space. By establishing the following optimization model, the cutting plane parameters corresponding to each subspace can be calculated.
Since the optimization model specifies that the error between the original function plane and the hyperplane is positive, the resulting linearized function is more conservative than the original high-order function, strictly satisfying the frequency safety constraint. The linearization error can be controlled by the number of subspaces. In this paper, is set as 100 and the relative error is less than 3%.
Therefore, the frequency safety margin can be determined by the minimum value of the product of frequency deviation and all approximate hyperplanes, as shown in the following equation: