How to Find the Moment of Inertia Tensor for Rotated Point Masses?

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Homework Help Overview

The discussion revolves around finding the moment of inertia tensor for a system of two point masses connected by a massless rod, initially positioned in a Cartesian coordinate system and later rotated in the OXY plane. Participants are tasked with calculating the tensor both before and after the rotation.

Discussion Character

  • Mixed

Approaches and Questions Raised

  • Participants explore the calculation of the moment of inertia tensor using relevant equations, questioning the correctness of their results and the contributions of various components.
  • There is discussion on the appropriate form of the rotation matrix and how it should be applied to the inertia tensor.
  • Some participants express uncertainty about the definitions and roles of the components in the inertia tensor, particularly regarding the distances involved.

Discussion Status

The conversation includes attempts to clarify the contributions to the inertia tensor and the proper application of the rotation matrix. Some participants agree on certain components being zero while others provide alternative perspectives on the calculations. There is no explicit consensus, but multiple interpretations and methods are being explored.

Contextual Notes

Participants are working under the constraints of homework rules, which may limit the information they can share or the methods they can use. There is also an emphasis on understanding the definitions and assumptions related to the moment of inertia tensor.

qoqosz
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Homework Statement


In Cartesian coordinate system are two point masses of mass [tex]m[/tex] connected with massless rod. Masses are in [tex](0,r,0)[/tex] and [tex](0,-r,0)[/tex].
a) Find the moment of inertia tensor.
b) Points were rotated in OXY plane such that angle between rod and Y-axis is [tex]\vartheta[/tex] (new cooridnates of masses are [tex](-r \sin \vartheta, r \cos \vartheta, 0)[/tex], [tex](r \sin \vartheta, -r \cos \vartheta, 0)[/tex]

Homework Equations


[tex]\hat{I} = \left(\begin{matrix}<br /> I_{xx} & I_{xy} & I_{xz}\\<br /> I_{yx} & I_{yy} & I_{yz}\\<br /> I_{zx} & I_{zy} & I_{zz}\\<br /> \end{matrix}<br /> \right)[/tex]
[tex]I_{xx} = \sum _{k} m_{k} (y^{2}_{k}+z^{2}_{k}) = \sum _{k} m_{k}(r^{2}_{k} - x^{2}_{k})\![/tex]
[tex]I_{yy} = \sum _{k} m_{k} (z^{2}_{k}+x^{2}_{k}) = \sum _{k} m_{k}(r^{2}_{k} - y^{2}_{k})\![/tex]
[tex]I_{zz} = \sum _{k} m_{k} (x^{2}_{k}+y^{2}_{k}) = \sum _{k} m_{k}(r^{2}_{k} - z^{2}_{k})\![/tex]
[tex]I_{xy} = I_{yx} = - \sum _{k} m_{k} x_{k}y_{k}\![/tex]
[tex]I_{yz} = I_{zy} = - \sum _{k} m_{k} y_{k}z_{k}\![/tex]
[tex]I_{zx} = I_{xz} = - \sum _{k} m_{k} z_{k}x_{k}\![/tex]


The Attempt at a Solution


a) Using relevant equations I get
[tex]\hat{I} = \left(\begin{matrix} 2 m r^2 & 0 & -2 m r^2 \\ 0 & 4 m r^2 & 0 \\ -2mr^2 & 0 & 2mr^2 \end{matrix}\right)[/tex]
is it correct?

b) I'm not sure, hence I'm asking :) - is it enough (and correct) to calculate:

[tex]\hat{I}' = \hat{I} \left(\begin{matrix} \cos \varphi & \sin \varphi & 0 \\ -\sin \varphi & \cos \varphi & 0 \\ 0 & 0 & 1 \end{matrix}\right)[/tex] or maybe [tex]\hat{I}' = \left(\begin{matrix} \cos \varphi & \sin \varphi & 0 \\ -\sin \varphi & \cos \varphi & 0 \\ 0 & 0 & 1 \end{matrix}\right) \hat{I}[/tex] or sth else?
 
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For a) I think there are only contributions in the top left and bottom right components.

Using your formulae, I_xy, I_xz and I_yz are all zero as they all involve multiplying by the x or z component of either particle's position (both of which are 0). Therefore all the off-diagonal entries must be 0. I agree with you for I_11 and I_33 however - I get both to be 2mr^2. However, the middle component, I_22, must be 0 as it's the sum of the square of the z component and the square of the x component but both x and z are 0 are mentioned previously.

To sum up, I get 2mr^2 in the top left and bottom right and 0's everywhere else.

Hope this helps.
 
b) wikipedia tells me the -ve signs should be the other way round in your rotation matrix for a rotation about the z axis (http://en.wikipedia.org/wiki/Rotation_matrix). Wikipedia calls this matrix R_z,theta, however we'll call it L. As your examining the moment of inertia tensor we need to use the transformation law for tensors:

I'_i,j=l_i,alpha*l_j,beta*I_alpha,beta

this implies that in terms of matrices, I'= L I L^T where L^T is the transpose of L

Just copmute that matrix product or you could repeat the process in a) using the new coordinates but this would be a bit tedious.

Let me know if this works. Also I'm new-ish here - how do you type in LaTeX?
 
Thanks for your replay.
But [tex]x_i[/tex] isn't x component of particle position but its distance to X-axis.
So for example [tex]I_{xz} = -m r \cdot r - m r \cdot r = - 2 mr^2[/tex]. Only [tex]y_i = 0[/tex] because both particles lie on Y-axis.

PS. To type in LaTeX use [tex]tags.[/tex]
 
Ok. Well I reckon my method for b) is still right.

Just reading my notes. I think that I_xx is the copmonent about the x axis.
r^2 - x^2 represents the perpendicular distance squared betweent he mass and the x axis.
but here x^2 is just the x component.
so y^2 + z^2 = r^2 - x^2 is just the sum of the squares of the y and z components and this represents the square of this perpendicular distance.

To see this, consider I_yy, as you dais both particles lie on the y axis, therefore there can be no moment of inertia about this axis and so I_yy=0
 
Last edited:
Ok, I was wrong. x_i is x component of mass position.
But in b) I think if L is a matrix of rotation there should be [tex]I' = L^T I L[/tex].
 
qoqosz said:
Thanks for your replay.
But [tex]x_i[/tex] isn't x component of particle position but its distance to X-axis.
Yes, it is. Another way to look at the inertia tensor for a collection of point masses about the origin is

[tex]\mathbf{I} = (\sum_k m_k\,r_k^2)\mathbf{1} - \sum_k m_k\,\mathbf {r}_k \mathbf {r}_k^T[/tex]

where [itex]\mathbf{1}[/itex] is the identity matrix, [itex]k[/itex] indexes the point masses, [itex]m_k[/itex] is the mass of the kth point mass, [itex]\mathbf {r}_k[/itex] are the coordinates of the kth point mass written as a column vector, and [itex]\mathbf {r}_k \mathbf {r}_k^T[/itex] is the outer product of that vector with itself. In terms of components, the above expression becomes

[tex]I_{ij} = \sum_k m_k(r_k^2\delta_{ij} - r_{k,i}r_{k,j})[/tex]


latentcorpse was exactly right in post #2. The only non-zero components of the inertia tensor for part (a) are Ixx and Izz.
 
qoqosz said:
Ok, I was wrong. x_i is x component of mass position.
But in b) I think if L is a matrix of rotation there should be [tex]I' = L^T I L[/tex].

Yes. You're correct here. That's what I was getting at but maybe it wasn't clear as I wasn't using LaTeX. However, in your original post, you only appear to have multiplied by one of the transormation matrices.
 
Ok, thank you both! :)
 

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