Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraft relative to Earth is = 1.6b +0.52b2+0.21bz (in rad/s). Now consider a top spinning in the spacecraft with an angular velocity relative to the spacecraft of wr = 5.86, +0.1962+0.15bg (in rad/s). What is the magnitude of the angular velocity (in rad/s) of the spinning top relative to the Earth reference frame. Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.

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Chapter1: Units, Trigonometry. And Vectors
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Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraft
relative to Earth is = 1.6b1 +0.52b2+0.21by (in rad/s). Now consider a top spinning in the
spacecraft with an angular velocity relative to the spacecraft of wr = 5.86, +0.19bg+0.15bg (in
rad/s). What is the magnitude of the angular velocity (in rad/s) of the spinning top relative to the
Earth reference frame.
Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.
Transcribed Image Text:Consider a spacecraft orbiting Earth. At an instant in time, the angular velocity of the spacecraft relative to Earth is = 1.6b1 +0.52b2+0.21by (in rad/s). Now consider a top spinning in the spacecraft with an angular velocity relative to the spacecraft of wr = 5.86, +0.19bg+0.15bg (in rad/s). What is the magnitude of the angular velocity (in rad/s) of the spinning top relative to the Earth reference frame. Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.
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