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Show that the initial conditions of the generalized coordinates \(q_{i}(t)\) can be expressed in terms of those of the physical coordinates \(x_{i}(t)\) in modal analysis as $$ \vec{q}(0)=[X]^{T}[m] \vec{x}(0), \quad \dot{\vec{q}}(0)=[X]^{T}[m] \dot{\vec{x}}(0). $$

Short Answer

Expert verified
To show the given expression, we follow these steps: 1. Convert generalized coordinates to physical coordinates using the relationship \(\vec{x}(t) = [X] \vec{q}(t)\), 2. Calculate the time derivatives of both coordinates, 3. Left-multiply both equations by the inverse of the mass matrix, [m]鈦宦, 4. Transpose the matrix of eigenvectors and left-multiply both equations by [X]岬, 5. Simplify the expressions using [X]岬[m]鈦宦筟X] = [I], 6. Obtain the initial conditions by setting t = 0. The resulting expressions are: $$ \vec{q}(0) = [X]^{T} [m]^{-1} \vec{x}(0) $$ and $$ \dot{\vec{q}}(0) = [X]^{T} [m]^{-1} \dot{\vec{x}}(0). $$

Step by step solution

01

Convert generalized coordinates to physical coordinates

We are given that the generalized coordinates, \(q_i(t)\), can be converted to physical coordinates, \(x_i(t)\), using the following relationship: $$ \vec{x}(t) = [X] [q](t) $$ where [X] is the matrix of eigenvectors.
02

Calculate the time derivatives of the coordinates

Next, we can find the relationship between the time derivatives of generalized coordinates and the physical coordinates. To do this, we take the time derivatives of both sides of the equation in Step 1: $$ \frac{d\vec{x}(t)}{dt} = [X] \frac{d\vec{q}(t)}{dt}. $$
03

Left-multiply both sides of the equation by the inverse of the mass matrix

The mass matrix, [m], is a diagonal matrix with the masses of each physical coordinate on the diagonal. Left-multiply both sides of the equations in Step 1 and Step 2 by the inverse of the mass matrix, [m]鈦宦: $$ [m]^{-1} \vec{x}(t) = [m]^{-1} [X] \vec{q}(t) $$ and $$ [m]^{-1} \frac{d\vec{x}(t)}{dt} = [m]^{-1} [X] \frac{d\vec{q}(t)}{dt}. $$
04

Transpose the matrix of eigenvectors

In order to achieve the desired expression, we need to obtain the transpose of the matrix of eigenvectors, [X]岬. By left-multiplying both sides of the equations in Step 3 by [X]岬, we get: $$ [X]^{T} [m]^{-1} \vec{x}(t) = [X]^{T} [m]^{-1} [X] \vec{q}(t) $$ and $$ [X]^{T} [m]^{-1} \frac{d\vec{x}(t)}{dt} = [X]^{T} [m]^{-1} [X] \frac{d\vec{q}(t)}{dt}. $$
05

Simplify the expressions

Since the product [X]岬[m]鈦宦筟X] = [I], the identity matrix, the equation simplifies to: $$ [X]^{T} [m]^{-1} \vec{x}(t) = \vec{q}(t) $$ and $$ [X]^{T} [m]^{-1} \frac{d\vec{x}(t)}{dt} = \frac{d\vec{q}(t)}{dt}. $$
06

Obtain the initial conditions

We can now express the initial conditions of the generalized coordinates and their time derivatives in terms of the physical coordinates and their time derivatives by setting t = 0. This gives us: $$ \vec{q}(0) = [X]^{T} [m]^{-1} \vec{x}(0) $$ and $$ \dot{\vec{q}}(0) = [X]^{T} [m]^{-1} \dot{\vec{x}}(0). $$ These are the expressions we were asked to show.

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Key Concepts

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

generalized coordinates
In modal analysis, generalized coordinates are variables that simplify the equations governing a physical system. Instead of dealing with potentially complicated physical coordinates, we use generalized coordinates like \( q_i(t) \) to express the system's behavior.
Generalized coordinates are particularly useful because they can be carefully chosen to match the modes of a mechanical system. These modes are specific patterns of motion the system naturally follows when disturbed. By using generalized coordinates that align with these modes, complex motion can be decoupled into simpler, independent motions.
This simplification arises because each generalized coordinate typically corresponds to a specific mode of vibration, allowing a focus on one mode at a time. This makes the analysis of a mechanical system more manageable, as opposed to dealing with every physical motion simultaneously.
physical coordinates
Physical coordinates \( x_i(t) \) represent the actual displacement of a mass in real space. They give a more direct depiction of where each part of a structure or system is at any given time.
In the context of mechanical systems, physical coordinates can be cumbersome, especially in multi-degree systems where several parts move in different directions at once. This is why converting to generalized coordinates is beneficial.
However, physical coordinates are essential as the starting point because they relate to the observable quantities that we can measure or track. They form the foundation for converting to generalized coordinates using a matrix of eigenvectors, as shown in modal analysis.
eigenvectors
Eigenvectors play a crucial role in modal analysis. They form the core of the matrix \( [X] \), which serves as a transformative tool between physical and generalized coordinates.
An eigenvector in the context of modal analysis is a special non-zero vector that only changes in scale, not direction, when a particular linear transformation (like a system's stiffness matrix) is applied.
These eigenvectors represent the inherent modes of the system, each associated with a specific frequency at which the system tends to naturally oscillate. By arranging these eigenvectors into a matrix, they enable the conversion between the two sets of coordinates, simplifying the analysis significantly.
In practice, once eigenvectors are determined, they assist in diagonalizing the system鈥檚 equations, transforming complex coupled equations into simpler, individual ones.
mass matrix
The mass matrix \( [m] \) is a diagonal matrix essential in dynamics, representing how mass is distributed across a mechanical system. Each diagonal element corresponds to the mass of a specific coordinate.
In modal analysis, the mass matrix plays a role in scaling and normalizing the transformation from physical to generalized coordinates. Because it is diagonal, it simplifies calculations significantly, allowing easy application of transformations.
During the conversion process, left-multiplying by the inverse of the mass matrix \( [m]^{-1} \) helps in normalizing these transformations. This process is crucial to relate the time derivatives of generalized and physical coordinates, ensuring all variables are correctly adjusted for the mass they influence.

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Most popular questions from this chapter

Consider the eigenvalue problem: $$\omega^{2}\left[\begin{array}{ll} 1 & 0 \\ 0 & 2 \end{array}\right]\left\\{\begin{array}{l} X_{1} \\ X_{2} \end{array}\right\\}=\left[\begin{array}{rr} 6 & -2 \\ -2 & 2 \end{array}\right]\left\\{\begin{array}{l} X_{1} \\ X_{2} \end{array}\right\\}$$ a. Find the natural frequencies and mode shapes of the system. b. Change the coordinates in Eq. (E.1) as \(X_{1}=Y_{1}\) and \(X_{2}=3 Y_{2}\) and express the eigenvalue problem in terms of the eigenvector \(\vec{Y}=\left\\{\begin{array}{l}Y_{1} \\ Y_{2}\end{array}\right\\}\), solve it, and find the natural frequencies and mode shapes. c. Compare the results found in parts (a) and (b) and give your observations.

Consider the eigenvalue problem $$\left[[k]-\omega^{2}[m]\right] \vec{X}=\overrightarrow{0}$$ where $$[m]=\left[\begin{array}{ll} 2 & 0 \\ 0 & 1 \end{array}\right] \text { and }[k]=\left[\begin{array}{cc} 8 & -4 \\ -4 & 4 \end{array}\right]$$ Find the natural frequencies and mode shapes of the system: a. by solving the equation \(\left[[m]^{-1}[k]-\omega^{2}[I]\right] \vec{X}=\overrightarrow{0}\) b. by solving the equation \(\left[-\omega^{2}[k]^{-1}[m]+[I]\right] \vec{X}=\overrightarrow{0}\) c. Compare the two sets of results and give your observations.

Using the MATLAB function roots, find the roots of the following equation: $$ f(x)=x^{12}-2=0 $$

Consider the eigenvalue problem: $$\lambda[m] \vec{X}=[k] \vec{X}$$ where $$[m]=\left[\begin{array}{ll} 1 & 0 \\ 0 & 4 \end{array}\right], \quad[k]=\left[\begin{array}{rr} 8 & -2 \\ -2 & 2 \end{array}\right], \quad \text { and } \quad \lambda=\omega^{2}$$ Equation (E.1) can be expressed as $$[D] \vec{X}=\lambda \vec{X}$$ where $$[D]=\left([m]^{\frac{1}{2}}\right)^{-1}[k]\left([m]^{\frac{1}{2}}\right)^{-1}$$ is called the mass normalized stiffness matrix. Determine the mass normalized stiffness matrix and use it to find the eigenvalues and orthonormal eigenvectors of the problem stated in Eq. (E.1).

Find and plot the response, \(x_{1}(t)\) and \(x_{2}(t),\) of a system with the following equations of motion: $$\left[\begin{array}{ll} 5 & 0 \\ 0 & 2 \end{array}\right]\left\\{\begin{array}{l} \ddot{x}_{1} \\ \ddot{x}_{2} \end{array}\right\\}+\left[\begin{array}{cc} 0.5 & -0.6 \\ -0.6 & 0.8 \end{array}\right]\left\\{\begin{array}{c} \dot{x}_{1} \\ \dot{x}_{2} \end{array}\right\\}+\left[\begin{array}{cc} 20 & -2 \\ -2 & 2 \end{array}\right]\left\\{\begin{array}{l} x_{1} \\ x_{2} \end{array}\right\\}=\left\\{\begin{array}{l} 1 \\ 0 \end{array}\right\\} \sin 2 t \quad \text { (E.1) }$$ using the initial conditions: $$\vec{x}(t=0)=\left\\{\begin{array}{c} 0.1 \\ 0 \end{array}\right\\} \mathrm{m} \quad \text { and } \quad \dot{\vec{x}}(t=0)=\left\\{\begin{array}{l} 0 \\ 1 \end{array}\right\\} \mathrm{m} / \mathrm{s}$$ Solve the differential equations, (E.1), numerically using a suitable MATLAB function.

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