Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraftrelative to Earth is ū = 1.6b1+0.77b2+0.39b3 and the angular acceleration of the spacecraft relativeto Earth is zero. Now consider a top spinning in the spacecraft with an angular velocity relative tothe spacecraft of wr = 8.5b1+0.15b2+0.19bz and angular acceleration relative to the spacecraft ofar = 0.03b1 +0.16b2+0.23b3. What is the magnitude of the angular acceleration of the spinningtop relative to the Earth reference frame.Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.

Given data, Angular velocity of the spacecraft relative to Earth :- ω→=1.6b^1+0.77b^2+0.39b^3…

Answered: Consider a spacecraft orbiting Earth.…

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