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Find the eigenvalues and eigenvectors of the following matrices.\(\left(\begin{array}{lll}3 & 2 & 4 \\ 2 & 0 & 2 \\ 4 & 2 & 3\end{array}\right)\)

Short Answer

Expert verified
Calculate the characteristic polynomial, solve for \(\lambda\) to find eigenvalues, and then solve \(A - \lambda I\) for each eigenvalue to find the eigenvectors.

Step by step solution

01

- Write Down the Characteristic Equation

The eigenvalues of a matrix are found by solving the characteristic equation. The characteristic equation is given by \(\det(A - \lambda I) = 0\), where \(A\) is the matrix and \(\lambda\) is the eigenvalue. For the given matrix \(A = \left(\begin{array}{lll}3 & 2 & 4 \ 2 & 0 & 2 \ 4 & 2 & 3\end{array}\right)\) and the identity matrix \(I\), calculate \(A - \lambda I\).
02

- Calculate \(A - \lambda I\)

Subtract \(\lambda\) times the identity matrix from \(A\): \[\left( \begin{array}{ccc} 3 & 2 & 4 \ 2 & 0 & 2 \ 4 & 2 & 3 \end{array} \right) - \lambda \left( \begin{array}{ccc} 1 & 0 & 0 \ 0 & 1 & 0 \ 0 & 0 & 1 \end{array} \right) = \left( \begin{array}{ccc} 3-\lambda & 2 & 4 \ 2 & -\lambda & 2 \ 4 & 2 & 3-\lambda \end{array} \right)\].
03

- Find the Determinant of \(A - \lambda I\)

Calculate the determinant of the matrix \(\left( \begin{array}{ccc} 3-\lambda & 2 & 4 \ 2 & -\lambda & 2 \ 4 & 2 & 3-\lambda \end{array} \right)\). Use the cofactor expansion method to find the determinant: \[\det(A - \lambda I) = \begin{vmatrix} 3-\lambda & 2 & 4 \ 2 & -\lambda & 2 \ 4 & 2 & 3-\lambda \end{vmatrix}= (3-\lambda) \begin{vmatrix} -\lambda & 2 \ 2 & 3-\lambda \end{vmatrix} - 2 \begin{vmatrix} 2 & 2 \ 4 & 3-\lambda \end{vmatrix} + 4 \begin{vmatrix} 2 & -\lambda \ 4 & 2 \end{vmatrix}\].
04

- Simplify the Determinant

Evaluate each determinant: \[\det(A - \lambda I) = (3-\lambda)[(-\lambda(3-\lambda) - 4)] - 2[(2(3-\lambda) - 8)] + 4[(2(-\lambda) - 8)]\]. Simplify further to get the characteristic polynomial in terms of \(\lambda\).
05

- Solve the Characteristic Polynomial

Solve the polynomial obtained in Step 4 for \(\lambda\). This will give the eigenvalues.
06

- Find the Eigenvectors

Substitute each eigenvalue \(\lambda_i\) back into the equation \(A - \lambda_i I\) and solve the resulting system of linear equations for the eigenvectors.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Characteristic Equation
To determine the eigenvalues of a matrix, start with the **characteristic equation**. This equation is derived by subtracting \( \lambda I \) from the matrix A, and then finding the determinant of the resulting matrix. The characteristic equation is given by \[ \det(A - \lambda I) = 0 \]. Here, \( A \) is the matrix in question, \( I \) is the identity matrix of the same dimensions as \( A \), and \( \lambda \) represents the eigenvalue. Solving this determinant equation yields the eigenvalues.
Determinant
Next, we need to find the determinant of the matrix \( A - \lambda I \). Given matrix \( A \), and identity matrix \( I \), first create the matrix \( A - \lambda I \) by subtracting \( \lambda <> I \) from each corresponding element of \( A \). The determinant of the resultant matrix is computed using methods such as cofactor expansion or Laplace's formula. For instance, for a 3x3 matrix, you expand along any row or column. Calculating these determinants step-by-step is crucial:
  • Write down the matrix \( A - \lambda I \).
  • Perform the row or column expansion to find sub-determinants.
  • Simplify to get a polynomial equation in \( \lambda \).
Remember, the solutions to this polynomial are the eigenvalues.
Eigenvector Calculation
Once the eigenvalues \( \lambda_i \) are found, the next task is to determine the corresponding eigenvectors. Insert each eigenvalue \( \lambda_i \) back into the expression \( (A - \lambda_i I) \mathbf{x} = 0 \), where \( \mathbf{x} \) is the eigenvector. This results in a homogeneous system of linear equations. Find this vector by:
  • Substituting \( \lambda_i \) into \( A - \lambda_i I \).
  • Solving the resulting equation system for the components of \( \mathbf{x} \).
Eigenvectors are typically normalized so that they have a length of 1, making them unique representations within their eigenspace.
Linear Algebra Methods
Linear Algebra provides the tools necessary to solve for eigenvalues and eigenvectors efficiently. Some common methods include:
  • **Matrix Decomposition Techniques:** Methods like QR decomposition can simplify the computation of eigenvalues and eigenvectors.
  • **Numerical Methods:** Algorithms such as the Power Method, Inverse Iteration, and the QR algorithm can find estimates of eigenvalues and eigenvectors, particularly useful for large matrices.
  • **Symbolic Computation:** Use of software (like MATLAB or Mathematica) can perform the algebraic manipulation needed to solve characteristic equations and determinants.
Applying these techniques helps to break down complex problems, making them easier to understand and solve.

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Most popular questions from this chapter

(a) If a body is rotating about a fixed axis, then its angular momentum \(L\) and its angular velocity \(\boldsymbol{o}\) are parallel vectors and \(\mathrm{L}=\mathrm{le} \mathrm{s}\), where \(I\) is the (scalar) moment of inertia of the body about the axis. However, in general, \(L\) and \(\omega\) are not parallel and \(I\) in the equation must be a second-order tensor; let us call it I. Find I in dyadic form in the following way: For simplicity, first consider a point mass \(m\) at the point \(r\). The angular momentum of \(m\) about the origin is by definition \(m r \times v\), where \(v\) is the linear velocity.From Chapter \(6, v=\omega \times r .\) Write out the triple vector product for \(L\) and from it write each component of \(\mathrm{L}\) in terms of the three components of 6 . Write your results in matrix form and in dyadic form $$ \mathbf{L}=\mathbf{I} \cdot \mathbf{\omega}=\left(\mathrm{ii} l_{x x}+\mathrm{ij} l_{x y}+\cdots\right)+\omega $$ You should have $$ I_{x z}=m\left(y^{2}+z^{2}\right), \quad I_{x y}=-m x y, \quad \text { etc. } $$ For a set of masses \(m_{i}\) or an extended body, replace the cxpressions for \(I_{z x+}, \operatorname{ctc}_{4}\), by the corresponding sums or integrals: $$ \begin{aligned} &I_{x x}=\sum m_{i}\left(y_{i}^{2}+z_{i}^{2}\right) \quad \text { or } \quad \int\left(y^{2}+z^{2}\right) d m_{4} \\ &I_{x y}=-\sum m_{j} x_{i} y_{i} \quad \text { or }-\int x y d m_{4} \quad \text { etc. } \end{aligned} $$ (b) Show that 1 is a second-order (Cartesian) tensor by expressing its components relative to a rotated system \(\left[I_{s^{\prime} x^{\prime}}=m\left(y^{2}+z^{\prime 2}\right)\right.\), etc. \(]\) in terms of \(x, y, z\) using \((11.7)\) or \((11.11)\), and hence in terms of \(I_{x \pi}\), etc., to show that I obeys the transformation equations \((11,13)\). (c) Show that if \(\mathrm{n}\) is a unit vector, the expression \(\mathbf{n}+\mathbf{1} \cdot \mathbf{n}\) gives the moment of inertia about an axis through the origin parallel to n. Hint: Consider I rotated to a system in which one of the axes is along \(n\). (d) Observe that the I matrix is symmetric and recall that a symmetric matrix may be diagonalized by a rotation of axes. The eigenvalues of the I matrix are called the principal moments of inertia. Show by part (c) that they are moments of inertia abour the new axes \(\left(x^{\prime}, y^{\prime}, z^{\prime}\right)\) relative to which \(\mathbf{I}\) is diagonal. These new axes are called the principal axes of incrtia. For the mass distribution consisting of point masses \(m\) at \((1,1,1)\) and \((1,1,-1)\), find the nine components of 1, and find the principal moments of inertia and the principal axes.

The characteristic equation for a second-order matrix \(M\) is a quadratic equation. We have, considered in detail the case in which \(M\) is a real symmetric matrix and the roots of thecharacteristic equation (eigenvalues) are real, positive, and unequal. Discuss some other possibilities as follows: (a) \(M\) real and symmetric, eigenvalues real, one positive and one negative. Show that the plane is reflected in one of the cigenvector lines (as well as stretched or shrunk). Consider as a simple special case $$ M=\left(\begin{array}{rr} 1 & 0 \\ 0 & -1 \end{array}\right) $$ (b) \(M\) real and symmetric, eigenvalues equal (and therefore real). Show that \(M\) must he a multiple of the unit matrix. Thus show that the deformation consists of dilation or shrinkage in the radial direction (the same in all directions) with no rotation (and reflection in the origin if the root is negative). (c) \(M\) real, not symmetric, eigenvalues real and not equal. Show that in this case the eigenvectors are not orthogonal. Hint: Find their dot product. (d) \(M\) real, not symmetric, eigenvalues complex, Show that all vectors are rotated, that is, there are no (real) eigenvectors which are unchanged in direction by the transformation. Consider the characteristic equation of a rotation matrix as a special case.

Rotate the given quadric surface to principal axes. What is the name of the surface? What is the shortest distance from the origin to the surface?\(7 x^{2}+4 y^{2}+z^{2}-8 x z=36\)

Find the eigenvalues and eigenvectors of the following matrices.\(\left(\begin{array}{lll}1 & 2 & 2 \\ 2 & 3 & 0 \\ 2 & 0 & 3\end{array}\right)\)

Find the inverse of the transformation $$ \begin{aligned} &x^{\prime}=2 x-3 y \\ &y^{\prime}=x+y \end{aligned} $$ that is, find \(x, y\) in terms of \(x^{\prime}, y^{\prime}\). (Hint : Use matrices.) Is the transformation orthogonal?

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