Math Problem Statement

solve it by control modern classic form

The state-space model of the system is given as: \[ \dot{x}(t) = \begin{bmatrix} 1 & \alpha & -2 \\ 0 & -2 & 0 \\ 0 & 1 & -1 \end{bmatrix} x(t) + \begin{bmatrix} -1 \\ 1 \\ 1 \end{bmatrix} u(t), \] \[ y(t) = \begin{bmatrix} 1 & 1 & 0 \end{bmatrix} x(t) \] (a) Find the value of \(\alpha\) such that the system becomes uncontrollable. (b) Using the value of \(\alpha\) obtained in part (a), derive the transfer function of the system and show that the system exhibits reduced-order dynamics.

Solution

To solve this problem, let's approach it step-by-step by using control theory concepts, specifically focusing on the controllability and transfer function of a state-space system.

Problem Analysis and Solution Steps:

Given System

The system's state-space representation is given by: x˙(t)=[1α2020011]x(t)+[111]u(t)\dot{x}(t) = \begin{bmatrix} 1 & \alpha & -2 \\ 0 & -2 & 0 \\ 0 & 1 & -1 \end{bmatrix} x(t) + \begin{bmatrix} -1 \\ 1 \\ 1 \end{bmatrix} u(t) y(t)=[110]x(t)y(t) = \begin{bmatrix} 1 & 1 & 0 \end{bmatrix} x(t)

The task is divided into two parts:

  1. Find the value of α\alpha that makes the system uncontrollable.
  2. With the value of α\alpha from part (a), derive the transfer function and show that the system exhibits reduced-order dynamics.

Step 1: Determine the Value of α\alpha for Uncontrollability

To determine controllability, we use the controllability matrix CC, defined as: C=[BABA2B]C = \begin{bmatrix} B & AB & A^2B \end{bmatrix} where AA is the system matrix, and BB is the input matrix. The system is controllable if the rank of CC is equal to the order of the system (in this case, 3).

Constructing the Controllability Matrix CC:

  1. Calculate BB, which is given directly.
  2. Compute ABAB and A2BA^2B.
  3. Form CC and evaluate its rank.

For uncontrollability, we need the rank of CC to be less than 3, which occurs if α\alpha satisfies certain conditions.


Step 2: Derive the Transfer Function for the Uncontrollable Case

With the determined value of α\alpha, we can find the transfer function G(s)=Y(s)U(s)G(s) = \frac{Y(s)}{U(s)} from the state-space representation by using the formula: G(s)=C(sIA)1B+DG(s) = C(sI - A)^{-1}B + D Here:

  • ss is the Laplace variable.
  • II is the identity matrix of appropriate dimensions.

Since we have no direct feedthrough (D=0D = 0), we only need to compute C(sIA)1BC(sI - A)^{-1}B.


Let's proceed with the calculations:

1. Calculate the Controllability Matrix and Find α\alpha for Uncontrollability

2. Derive the Transfer Function with the Identified α\alpha

I'll compute these values step-by-step and present the results.The rank of the controllability matrix CC is 3 for general values of α\alpha, indicating that the system is generally controllable. However, we need the system to become uncontrollable, which would occur if the rank of CC drops below 3.

To achieve this, we need to find specific values of α\alpha that make the columns of CC linearly dependent, causing the rank to drop.

Let's proceed by setting conditions for linear dependence in CC to identify values of α\alpha that would make the system uncontrollable.It seems there was an issue with computing the determinant directly. Instead, I'll try examining linear dependencies among columns of the controllability matrix to identify values of α\alpha that result in a rank deficiency.

I'll check for conditions on α\alpha by analyzing dependencies in the columns of CC rather than relying solely on the determinant approach.The reduced row echelon form (RREF) of the controllability matrix CC confirms that, for general values of α\alpha, the system remains controllable, as the RREF has full rank (3). This implies that there is no value of α\alpha for which the system naturally becomes uncontrollable with the given form of AA and BB.

If you're specifically interested in an analysis for reduced-order dynamics, I could proceed with computing the transfer function directly using symbolic values and illustrate any conditions that might suggest reduced-order behavior.

Would you like me to continue with the transfer function computation under this assumption?

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Math Problem Analysis

Mathematical Concepts

Control Theory
State-Space Representation
Controllability
Transfer Function
Linear Algebra

Formulas

Controllability Matrix: C = [B, AB, A^2B]
Transfer Function: G(s) = C(sI - A)^(-1)B + D

Theorems

Controllability Theorem
State-Space to Transfer Function Conversion

Suitable Grade Level

Undergraduate (Engineering - Control Systems)