Coupled Oscillator: Pulley: Difference between revisions
(New page: ==Coupled Oscillator: Pulley System== ===Problem=== Given the system shown, with all initial positions set so that gravity is accounted for and no motion is occurring, find the response. ...) |
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<math>\sum F=ma </math> |
<math>\sum F=ma </math> |
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<math>-k_1x_1- |
<math>-k_1x_1-k_2(x_1-x_2)=m_1\ddot{x_1}</math> |
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<math>\dfrac{-x_1(k_1+k_2)}{m_1}=\ddot{x_1}</math> |
<math>\dfrac{-x_1(k_1+k_2)-x_2k_2}{m_1}=\ddot{x_1}</math> |
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On the right, we have |
On the right, we have |
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<math>\sum F=ma </math> |
<math>\sum F=ma </math> |
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<math> |
<math>-k_2(x_2-x_1)=m_2\ddot{x_2}</math> |
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<math>\dfrac{ |
<math>\dfrac{-k_2(x_2-x_1)}{m_2}=\ddot{x_2}</math> |
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So, our state space matrices are |
So, our state space matrices are |
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= |
= |
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\begin{bmatrix} |
\begin{bmatrix} |
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0 & -\dfrac{k_1+k_2}{m_1} & 0 & |
0 & -\dfrac{k_1+k_2}{m_1} & 0 & -\dfrac{k_2}{m_1} \\ |
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1 & 0 & 0 & 0 \\ |
1 & 0 & 0 & 0 \\ |
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0 & |
0 & \dfrac{k_2}{m_2} & 0 & -\dfrac{k_2}{m_2} \\ |
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0 & 0 & 1 & 0 \\ |
0 & 0 & 1 & 0 \\ |
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\end{bmatrix} |
\end{bmatrix} |
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= |
= |
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\begin{bmatrix} |
\begin{bmatrix} |
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0 & -6 & 0 & |
0 & -6 & 0 & -5 \\ |
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1 & 0 & 0 & 0 \\ |
1 & 0 & 0 & 0 \\ |
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0 & |
0 & 2.5 & 0 & -2.5 \\ |
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0 & 0 & 1 & 0 \\ |
0 & 0 & 1 & 0 \\ |
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\end{bmatrix} |
\end{bmatrix} |
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Using any number of different computer utilities, we can calculate the eigenvalues and eigenvectors of the coefficient matrix quickly and easily. |
Using any number of different computer utilities, we can calculate the eigenvalues and eigenvectors of the coefficient matrix quickly and easily. |
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<math>\lambda_1=j2. |
<math>\lambda_1=0.705+j2.179</math><br> |
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<math>\lambda_2=-j2. |
<math>\lambda_2=0.705-j2.179</math><br> |
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<math>\lambda_3= |
<math>\lambda_3=-0.705+j2.179</math><br> |
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<math>\lambda_4=- |
<math>\lambda_4=-0.705-j2.179</math><br><br> |
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<math>k_1 \varpropto \begin{bmatrix} 0. |
<math>k_1 \varpropto \begin{bmatrix} 0.748 \\ 0.101-j0.311 \\ -0.262-j0.460 \\ -0.226+j0.047 \\ \end{bmatrix}</math><br> |
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<math>k_2 \varpropto \begin{bmatrix} 0. |
<math>k_2 \varpropto \begin{bmatrix} 0.748 \\ 0.101+j0.311 \\ -0.262+j0.460 \\ -0.226-j0.047 \\ \end{bmatrix}</math><br> |
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<math>k_3 \varpropto \begin{bmatrix} 0 \\ 0 \\ 0. |
<math>k_3 \varpropto \begin{bmatrix} 0.748 \\ -0.101-j0.311 \\ -0.262+j0.460 \\ 0.226+j0.047 \\ \end{bmatrix}</math><br> |
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<math>k_4 \varpropto \begin{bmatrix} 0 \\ 0 \\ -0. |
<math>k_4 \varpropto \begin{bmatrix} 0.748 \\ -0.101+j0.311 \\ -0.262-j0.460 \\ 0.226-j0.047 \\ \end{bmatrix}</math> |
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The full solution is |
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<math>\bar{x}=c_1k_1e^{\lambda_1 t}+c_2k_2e^{\lambda_2 t}+c_3k_3e^{\lambda_3 t}+c_4k_4e^{\lambda_4 t}</math> |
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===Eigenmodes=== |
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The four distinct eigenvalues mean there will be four eigenmodes (though two are similar). They are |
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1. The two masses moving in the same direction at all times (i.e. one up and the other down). |
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2. The two masses moving in opposite directions at all times (i.e. both up or down). |
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3. and 4. The masses moving at plus or minus 90 degrees of phase offset. |
Revision as of 20:49, 14 December 2009
Coupled Oscillator: Pulley System
Problem
Given the system shown, with all initial positions set so that gravity is accounted for and no motion is occurring, find the response. The spring around the pulley is modeled as a single spring with constant .
Solution
We begin by writing the sum of forces equations for both blocks.
On the left, we have
On the right, we have
So, our state space matrices are
Now, suppose we impose the initial conditions as follows:
=10 kg
=20 kg
=10 N/m
=50 N/m
We now have
Using any number of different computer utilities, we can calculate the eigenvalues and eigenvectors of the coefficient matrix quickly and easily.
The full solution is
Eigenmodes
The four distinct eigenvalues mean there will be four eigenmodes (though two are similar). They are
1. The two masses moving in the same direction at all times (i.e. one up and the other down). 2. The two masses moving in opposite directions at all times (i.e. both up or down). 3. and 4. The masses moving at plus or minus 90 degrees of phase offset.