Consider the matrices
\( M = \begin{pmatrix}
2 & 1 \\
0 & 2
\end{pmatrix} \)
\( N = \begin{pmatrix}
1 & 0 & 0 \\
1 & 2 & 0 \\
1 & 1 & 0
\end{pmatrix} \)
Which one of the following is true?
Step 1: Analyze the diagonalizability of \( M \).
Matrix \( M \) is \[ \begin{pmatrix} 2 & 1 \\ 0 & 2 \end{pmatrix}. \] The eigenvalues of \( M \) are \( \lambda = 2 \) with algebraic multiplicity 2. To check diagonalizability, compute the eigenvectors: \[ M - 2I = \begin{pmatrix} 0 & 1 \\ 0 & 0 \end{pmatrix}. \] The rank of \( M - 2I \) is 1, so the geometric multiplicity of eigenvalue \( \lambda = 2 \) is 1. Since the geometric multiplicity is less than the algebraic multiplicity, \( M \) is not diagonalizable.
Step 2: Analyze the diagonalizability of \( N \).
Matrix \( N \) is \[ \begin{pmatrix} 1 & 0 & 0 \\ 1 & 2 & 0 \\ 1 & 1 & 0 \end{pmatrix}. \] The eigenvalues of \( N \) are obtained by solving \( \det(N - \lambda I) = 0 \): \[ \det \begin{pmatrix} 1 - \lambda & 0 & 0 \\ 1 & 2 - \lambda & 0 \\ 1 & 1 & -\lambda \end{pmatrix} = 0. \] Expanding the determinant: \[ (1 - \lambda)\left((2 - \lambda)(-\lambda)\right) = 0. \] This gives \( \lambda = 1, \lambda = 2, \lambda = 0 \). All eigenvalues of \( N \) have linearly independent eigenvectors (verified through eigenvector computation). Therefore, \( N \) is diagonalizable.
Step 3: Conclusion.
Matrix \( M \) is not diagonalizable due to insufficient independent eigenvectors, while \( N \) is diagonalizable.
A ship with a standard right-handed coordinate system has positive \(x\), \(y\), and \(z\) axes respectively pointing towards bow, starboard, and down as shown in the figure. If the ship takes a starboard turn, then the drift angle, sway velocity, and the heel angle of the ship for a steady yaw rate respectively are: 
The GZ curve for a stable ship is shown in the figure, where \( P \) is a point of inflection on the curve. Match the labels in Column 1 with the corresponding descriptions in Column 2. 
A ship with a standard right-handed coordinate system has positive \(x\), \(y\), and \(z\) axes respectively pointing towards bow, starboard, and down as shown in the figure. If the ship takes a starboard turn, then the drift angle, sway velocity, and the heel angle of the ship for a steady yaw rate respectively are: 
The GZ curve for a stable ship is shown in the figure, where \( P \) is a point of inflection on the curve. Match the labels in Column 1 with the corresponding descriptions in Column 2. 