How Is This Torque Equation Derived?

  • Thread starter Thread starter Thales
  • Start date Start date
  • Tags Tags
    Torque
AI Thread Summary
The discussion centers on the torque equation for a rigid body, specifically the equation involving angular momentum around the center of gravity (CG) and its relationship to inertia and angular velocity. The original poster seeks a derivation of this equation, expressing confusion about its meaning. A contributor suggests that the derivation likely involves concepts from noninertial reference frames, particularly focusing on rotating coordinate systems. They mention finding a similar derivation in their dynamics text, which generalizes the equation for arbitrary vectors and connects it to Euler's equations for rigid bodies. Another participant expresses interest in receiving the proof, which is available in the contributor's lecture notes, although not in English. The conversation also touches on the time derivative of body-fixed unit coordinate vectors and how they relate to the absolute time derivative of vectors expressed in body coordinates, emphasizing the mathematical relationships involved in rotational dynamics.
Thales
Messages
13
Reaction score
0
I have this book, which provides the following torque equation for a rigid body:

\sum\tau_{cg} = \frac{dL_{cg}}{dt} = I\frac{d\omega}{dt} + (\omega \times (I\omega))

Where L_{cg} is the angular momentum around the CG. The moments, inertia tensor, and angular velocity are all expressed in local (body) coordinates.

This is all fine and dandy, but what is not provided is a derivation. I'm wondering if anyone knows its derivation, because I don't fully understand its meaning. :rolleyes:

Any help would be greatly appreciated.

Thanks!
 
Physics news on Phys.org
I believe the answer has something to do with the fact you are dealing with motion in a noninertial reference frame. You may be dealing with "fixed" axes and "rotating" axes. The derivation may lie in the section pertaining to rotating coordinate systems under the noninertial reference frames chapter. For example, in my dynamics text I found a derivation for an equation matching the one you show, except that it was generalized for an arbitrary vector. In other words, just replace your vector Lcg and I(omega), which are equivalent, with a general vector and you get the equation in my book. This equation was later used with torque when dealing with Euler's equations for a rigid body. Hope this helps.

BTW I would have given you the equation in my book directly, however, I do not yet know how to input formulas in this forum yet!
 
I know it, but it's long and boring. Beleive me, you're not missing anything crucial. If you want the proof I have it complete in my lecture notes. They are not in English, but I think you would have no problem understanding the proof. If you are interesting I can email you the doc.
 
Thanks to both of you for the feedback.

quarkman, if you want to learn about using latex, check out:

Latex


tomkeus, even if it's boring, I'd love to see it. :biggrin:

I'm not sure if this forum provides an email attachment capability... But you can send it to jwalway@hotmail.com

Thanks again!
 
I have sent it.
 
Given a set of body-fixed unit coordinate vectors
\vec{i}_{x,b},\vec{i}_{y,b},\vec{i}_{z,b}
for a body that rotates absolutely with \vec{\omega},
the time change of these absolutely is given by:
\frac{d\vec{i}_{x,b}}{dt}_{abs}=\vec{\omega}\times\vec{i}_{x,b}
and similarly for the two others.
(Clearly, this is a statement, not a proof, but ought to be obvious)

Let a vector be given in body coordinates:
\vec{L}=L_{x}\vec{i}_{x,b}+L_{y}\vec{i}_{y,b}+L_{z}\vec{i}_{z,b}
Hence, the absolute time derivative is given by:
\frac{d\vec{L}}{dt}_{abs}=\frac{d\vec{L}}{dt}_{rel}+\vec{\omega}\times\vec{L}
Here, we have the relative time derivative (i.e, in which the axes is considered fixed):
\frac{d\vec{L}}{dt}_{rel}=\frac{dL_{x}}{dt}\vec{i}_{x,b}+\frac{dL_{y}}{dt}\vec{i}_{y,b}+\frac{dL_{z}}{dt}\vec{i}_{z,b}
 
Back
Top