Space Vehicle Dynamics 🚀 Lecture 19, part 1: Moment of inertia matrix (inertia tensor) and the principal axis frame. We discuss the calculation of the moment of inertia matrix for a rigid body and its properties. The eigenvalues of this matrix are the principal moments of inertia and the corresponding eigenvectors are the principal axes of rotation, special directions about which the rigid body can freely rotate in pure rotation (no wobbling). The transformation of the inertia matrix from one rigid body frame to another is given via the rotation matrix (direction cosine matrix).
We numerically demonstrate with a Matlab example. Starting with an inertia matrix, we find the principal moments and principal axes, and construct the principal axis frame.
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► References
Schaub & Junkins📘Analytical Mechanics of Space Systems, 4th edition, 2018
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► Chapters
0:00 Rigid body dynamics, continuous mass distribution
5:03 Moment of inertia matrix entries, integral over body
12:00 Principal axis frame -- easiest, most natural, rigid body frame
16:38 Transforming moment of inertia matrix between frames
19:26 How long does a potato stay fresh?
19:37 Principal axis frame, how to find it
25:24 MATLAB example of finding principal axis frame
32:19 Principal axes physical significance
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Негізгі бет Moment of Inertia Matrix & Principal Axis Frame | MATLAB Example Calculation
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