The large satellite-tracking antenna has a momentof inertia I about its z-axis of
Chapter 7, Problem 7/81(choose chapter or problem)
The large satellite-tracking antenna has a moment of inertia I about its z-axis of symmetry and a moment of inertia \(I_{O}\) about each of the x- and y-axes. Determine the angular acceleration \(\alpha\) of the antenna about the vertical Z-axis caused by a torque M applied about Z by the drive mechanism for a given orientation \(\theta\).
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