The design of control laws for MIMO systems are more extensive in comparison to SISO systems because the additional inputs () offer more options like defining the Eigenvectors or handling the activity of inputs. This also means that the feedback matrix K for a set of desired Eigenvalues of the closed-loop system is not unique.
All presented methods have advantages, disadvantages and certain limitations. This means not all methods can be applied on every possible system and it is important to check which method could be applied on the own considered problem.
A simple approach to find the feedback matrix K can be derived via parametric state feedback (in German: vollständige modale Synthese).
A MIMO system
with input vector
input matrix and feedback matrix is considered. The Eigenvalue problem of the closed-loop system
is noted as
where denote the assigned Eigenvalues and denote the Eigenvectors of the closed-loop system.
Next, new parameter vectors are introduced and assigned and the Eigenvalue problem is recasted as
1. From Equation [1] one defines the Eigenvector with
2. The new parameter vectors are concatenated as
where the feedback matrix K can be noted as
3. Finally, the Eigenvector definition is used to hold the full description of the feedback matrix with
The parameter vectors are defined arbitrarily but have to be linear independent.
- Method works for non-quadratic B
- Parameter vectors can be chosen arbitrarily
Consider the dynamical system
which is unstable due to positive Eigenvalues . A feedback matrix K should be found to reach a stable closed-loop system with Eigenvalues .
1. The parameter vectors are defined as and
2. The resulting Eigenvectors are
and
3. The feedback matrix is calculated with
More precise rounding leads to a feedback matrix
If the state matrix of system
is diagonalizable, which means the number of Eigenvalues and Eigenvectors are equal, then the transform
can be used to yield
and further
Transformation matrix M contains the Eigenvectors as
which leads to a new diagonal state matrix
consisting of Eigenvalues , and new input
The control law for the new input is designed as
and the closed-loop system in new coordinates is noted as
Feedback matrix can be used to influence or shift each Eigenvalue directly.
In the last step, the new input is transformed backwards to original coordinates to yield the original feedback matrix K. The new input is defined by
and
From these formulas one gains the identity
and further
Therefore, the feedback matrix is found as
This controller design is applicable only if the following requirements are guaranteed.
- State matrix A is diagonalizable.
- The number of states and inputs are equal .
- Input matrix is invertible.
Consider the dynamical system
which is unstable due to positive Eigenvalues . The Eigenvectors are
and
Thus, the transformation matrix is noted as
and the state matrix in new coordinates is derived as
The desired Eigenvalues of the closed-loop system are and , so feedback matrix is found with
and
and thus one holds
Finally, the feedback matrix in original coordinates are calculated by
This method is taken from the online resource
Consider the closed-loop system
with input and closed-loop state matrix .
The desired closed-loop Eigenvalues can be chosen real- or complex-valued as and the matrix of the desired Eigenvalues is noted as
The closed-loop state matrix has to be similar to as
which means that there exists a transformation matrix such that
holds and further
An arbitrary Matrix is introduced and Equation [2] is separated in a Sylvester equation
and a feedback matrix formula
1. Choose an arbitrary matrix .
2. Solve the Sylvester equation for M (numerically).
3. Calculate the feedback matrix K.
- State matrix A and the negative Eigenvalue matrix shall not have common Eigenvalues.
- For some choices of G the computation could fail. Then another G has to be chosen.
Consider the dynamical system
which is unstable due to positive Eigenvalues . The complex-valued Eigenvalues are desired for the closed-loop system. So, the eigenvalue matrix is noted as
Matrix G is chosen as
and Sylvester equation
is noted. The Sylvester equation is solved numerically and the transformation matrix is computed as
Finally, the feedback matrix is found as