Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraftrelative to Earth is = 1.9bh +0.82b2+0.34b3 (in rad/s) and the angular acceleration of thespacecraft relative to Earth is a = 0.0561 +0.19bz+0.22bg (in rad/s?). What is the moment (in N.m)being applied on the spacecraft in the b2.Assume the moment of inertia of the spacecraft is given by:Г50000.00.00.0 100000.0kg.m?0.013000Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.

Given: The angular velocity of the spacecraft relative to the Earth is ω→ = 1.9 b^1 + 0.82 b^2 +…

Answered: Consider a spacecraft orbiting Earth.…

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