Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraftrelative to Earth is ū = 1.161+0.58b2+0.5b3 and the angular acceleration of the spacecraft relativeto Earth is a = 0.04b1 +0.11b2+0.26b3. What is the moment being applied on the spacecraft in theb2.Assume the moment of inertia of the spacecraft is given by:50000.00.0[I°] =kg.m20.0100000.00.013000Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.

The Moment of a force is the tendency of the force to rotate an object with respect to a fixed…

Answered: Consider a spacecraft orbiting Earth.…

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