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Full-state feedback control designСодержание книги
Поиск на нашем сайте FULL-STATE FEEDBACK CONTROL DESIGN
In this section, we consider full-state variable feedback to achieve the desired pole locations of the closed-loop system.
FIGURE 46.1 State variable compensator employing full-state feedback in series with a full-state observer.
A key question that arises in the design of state variable compensators is whether or not all the poles of the closed-loop system can be arbitrarily placed in the complex plane. Recall that the poles of the closed-loop system are equivalent to the eigenvalues of the system matrix in state variable format. As we shall see, if the system is controllable and observable, then we can accomplish the design objective of placing the poles precisely at the desired locations to meet the performance specifications. Full-state feedback design commonly relies on pole-placement techniques. It is important to note that a system must be completely controllable and completely observable to allow the flexibility to place all the closed-loop system poles arbitrarily.
Full state feedback (FSF), or pole placement, is a method employed in feedback control system theory to place the closed-loop poles of a plant in pre-determined locations in the s-plane. Placing poles is desirable because the location of the poles corresponds directly to the eigenvalues of the system, which control the characteristics of the response of the system. The system must be considered controllable in order to implement this method.
If the closed-loop input-output transfer function can be represented by a state space equation, see State space (controls),
then the poles of the system are the roots of the characteristic equation given by
Full state feedback is utilized by commanding the input vector
Substituting into the state space equations above,
The roots of the FSF system are given by the characteristic equation, Example 46.1 Consider a control system given by the following state space equations
The uncontrolled system has closed-loop poles at s = − 1 and s = − 2. Suppose, for considerations of the response, we wish the controlled system eigenvalues to be located at s = − 1 and s = − 5. The desired characteristic equation is then s 2 + 6 s + 5 = 0. Following the procedure given above,
Upon setting this characteristic equation equal to the desired characteristic equation, we find
Therefore, setting
Determining the gain matrix K is the objective of the full-state feedback design procedure. The beauty of the state variable design process is that the problem naturally separates into a full-state feedback component and an observer design component. These two design procedures can occur independently, and in fact, the separation principle provides the proof that this approach is optimal. We will show later that the stability of the closed-loop system is guaranteed if the full-state feedback control law stabilizes the system (under the assumption of access to the complete state) and the observer is stable (the tracking error is asymptotically stable). Observer design will be discussed in Lecture 4.7.
Example 46.2 Let’s consider a 3rd order control system which is described by the following differential equation
We may choose the following state variables
Then we may describe this system in matrix form
and
If the state variable feedback matrix is
and
then the closed-loop system is
The state feedback matrix is
and the characteristic equation is
If we seek a rapid response with a low overshoot, we choose a desired characteristic equation such as (see Equation 5.18 and Table 5.2)
We choose If we want a settling time (with a 2% criterion) equal to 1 second, then
If we choose
Comparing Equations (46.1) and (46.2) yields the three equations
Therefore, we require that
Example 46.3 Let’s consider a control system with full-state feedback control (output variable This system is using a DC motor which is controlled by an exciting circuit. The transfer function of this DC motor is as follows
where We suppose that As you may see from Fig.46.2 the control system has 3 feedback loops: on position, motor speed, and excitation current. Suppose, that the coefficient of feedback loop on position is equal to -1 (look at Fig.46.3).
Fig.46.2 A control system with full-state feedback control (output variable
Ackermann’s formula
Example 46.4 Let’s consider a compensator design problem for a satellite control system.
Example 46.5 Let’s consider a compensator design problem for a satellite control system from the previous example. The state-space model is as follows
The desirable characteristic equation is as follows
In order to define K matrix we use the Ackermann’s formula.
then
We may define a matrix polynomial
Then we apply the Ackermann’s formula
Thus, the sought coefficient feedback matrix has the following form
We obtained the result which coincides with the previous example.
Example 46.6 We continue to consider the system which controls a satellite. Suppose, that according to requirements it’s necessary to obtain a critically damped system with the settling time 1 s, i.e. In this case the desired characteristic equation will be as follows
FULL-STATE FEEDBACK CONTROL DESIGN
In this section, we consider full-state variable feedback to achieve the desired pole locations of the closed-loop system.
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