Gyroscope precession derivation

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SUMMARY

The discussion focuses on the derivation of gyroscope precession, specifically addressing the application of torque when a small force is applied to a rotating body. The user describes the scenario where the body rotates about a principal axis with a constant angular velocity, represented by the rotation vector w equal to e(3). The user seeks clarification on the step involving the equation J(dot) = I(3)w(dot) = r x F, which relates the change in angular momentum to the applied force and its lever arm. The conversation highlights the importance of understanding the inertia tensor and its role in rigid body dynamics.

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  • Familiarity with the inertia tensor and principal axes
  • Knowledge of angular momentum and torque concepts
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bman!!
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alrite I am new on this forum...just discovered it...pretty awesome

ok, I am looking over notes from a classical physics course i did, and I've just covered rigid bodies, and literally just got through the inertia tensor, principal axes and all that good stuff.

there's a step in the gyroscope precession, that is mathematically very simple, but I am just having a brain fart and it completely eludes me:

body is roating about a principle axis such that w (rotation vector) is equal to we(3) where e(3) is the principle axes of the body vector (presumably the vector that is perpendicular to the face of the spinning disk)

this means ang mom J=I(3)we(3) where I(3) is the corresponding moment of inertia.

thus the differential of this quantity to get the torque is therefore = 0 as w is constant.

i understand this...but then

small force F is applied somewhere along this axis at r, this force is perpendicular to w. the body then acquires small component of angular v perpendicular to its axis, new equation of motion, the torque ;J(dot) = r x F.

i also understand this bit, but then this next simple step completely throws me;

if the force is small, the new angular velocity component will be small compared to the angular velocity of the orignal rotation,we can then ignore angular momentum components normal to the axis and therefore write

J(dot) = I(3)w(dot) = r x F

i just do not understand this bit.

if the notation comfuses I've attached the source notes from where I am revising. the section is on pages 17-18, the notes are good, but i have to say the inertai tensor bit was somewhat lacking in explanation for my taste.

i realize forum etiquette requires i look at old posts and all that, but this quite specific question about a step in a derviation that i simply do not get.

any help appreciated.

cheers
 

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id also like to add, i didnt think this was quite homework and coursework, so i posted it here, cos it was difficulty in conceptualising rather than raw calculation difficulty
 
uhhhh brain fart, i think i just got it...

i feel like a retard.
 

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