Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraftrelative to Earth is = 1.6b +0.52b2+0.21b3 (in rad/s). Now consider a top spinning in thespacecraft with an angular velocity relative to the spacecraft of wr = 5.86, +0.19bz+0.15bz (inrad/s). What is the magnitude of the angular velocity (in rad/s) of the spinning top relative to theEarth reference frame.Note b1, b2, by are unit vectors fixed in the spacecraft reference frame.

Given, The angular velocity of spacecraft with respect to earth is, ω→=1.6b^1+0.52b^2+0.21b^3 rad/s…

Answered: Consider a spacecraft orbiting Earth.…

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