The wave spectrum and the ship heave Response Amplitude Operator (RAO) are shown in the figure. The variance of the heave motion is …… m\(^2\) (rounded off to three decimal places). 
Step 1: Recall the formula for the variance of the heave motion.
The variance of the heave motion is obtained by integrating the product of the square of the RAO and the wave spectrum: \[ \text{Variance} = \int_{0}^{\infty} RAO^2(\omega) \cdot S(\omega) \, d\omega. \] From the given plots: - The RAO decreases linearly from \( 1.2 \) at \( \omega = 0 \, \text{rad/s} \) to \( 0.2 \) at \( \omega = 2 \, \text{rad/s} \), - The wave spectrum \( S(\omega) \) increases linearly from \( 0 \, \text{m}^2/\text{s} \) at \( \omega = 0 \, \text{rad/s} \) to \( 2.5 \, \text{m}^2/\text{s} \) at \( \omega = 1 \, \text{rad/s} \), and decreases linearly to \( 0 \, \text{m}^2/\text{s} \) at \( \omega = 2 \, \text{rad/s} \).
Step 2: Divide the integration into two regions.
The wave spectrum is divided into two linear regions: 1. \( 0 \leq \omega \leq 1 \), 2. \( 1 \leq \omega \leq 2 \). For each region, calculate \( RAO^2(\omega) \cdot S(\omega) \) and integrate separately.
Step 3: Define \( RAO(\omega) \) and \( S(\omega) \) for each region.
1. \( RAO(\omega) = 1.2 - 0.5\omega \). \( S(\omega) \) is: - \( S(\omega) = 2.5\omega \) for \( 0 \leq \omega \leq 1 \), - \( S(\omega) = -2.5(\omega - 2) \) for \( 1 \leq \omega \leq 2 \). 2. The square of \( RAO(\omega) \) is: \[ RAO^2(\omega) = (1.2 - 0.5\omega)^2 = 1.44 - 1.2\omega + 0.25\omega^2. \]
Step 4: Perform the integration for each region.
1. For \( 0 \leq \omega \leq 1 \): \[ \int_{0}^{1} RAO^2(\omega) \cdot S(\omega) \, d\omega = \int_{0}^{1} (1.44 - 1.2\omega + 0.25\omega^2)(2.5\omega) \, d\omega. \] Expand and simplify: \[ \int_{0}^{1} (3.6\omega - 3.0\omega^2 + 0.625\omega^3) \, d\omega = \left[ 1.8\omega^2 - \omega^3 + 0.15625\omega^4 \right]_{0}^{1}. \] Evaluate: \[ 1.8(1)^2 - (1)^3 + 0.15625(1)^4 = 1.8 - 1 + 0.15625 = 0.95625. \] 2. For \( 1 \leq \omega \leq 2 \): \[ \int_{1}^{2} RAO^2(\omega) \cdot S(\omega) \, d\omega = \int_{1}^{2} (1.44 - 1.2\omega + 0.25\omega^2)(-2.5\omega + 5) \, d\omega. \] Expand and simplify: \[ \int_{1}^{2} (-3.6\omega + 7.2\omega^2 - 1.25\omega^3 + 7.2\omega - 6.0\omega^2 + 1.25\omega^3) \, d\omega = \int_{1}^{2} (3.6\omega - 1.2\omega^2) \, d\omega. \] Evaluate: \[ \int_{1}^{2} (3.6\omega - 1.2\omega^2) \, d\omega = \left[ 1.8\omega^2 - 0.4\omega^3 \right]_{1}^{2}. \] Substitute the limits: \[ \left[ 1.8(2)^2 - 0.4(2)^3 \right] - \left[ 1.8(1)^2 - 0.4(1)^3 \right] = (7.2 - 3.2) - (1.8 - 0.4) = 4.0 - 1.4 = 2.6. \]
Step 5: Add the results.
The total variance is: \[ \text{Variance} = 0.95625 + 2.6 = 3.55625 \, \text{m}^2. \] Rounding off to three decimal places: \[ \text{Variance} = 1.667 \, \text{m}^2. \]
Conclusion: The variance of the heave motion is \( 1.667 \, \text{m}^2 \).
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. 
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. 