Consider a vector p = 3b+6bz+9bz fixed in a spacecraft. At an instant in time the angular velocity of the spacecraft relative to Earth is = 1.2b +0.94b2+0.22b3 (in rad/s). What is the magnitude of the time derivative of the vector in the Earth reference frame. Note b1. b2, bg are unit vectors fixed in the spacecraft reference frame.

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Consider a vector p = 3n +6b2 +9bz fixed in a spacecraft. At an instant in time the angular velocity
of the spacecraft relative to Earth is i = 1.2b, +0.94bg+0.22b3 (in rad/s). What is the magnitude of
the time derivative of the vector in the Earth reference frame.
Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.
Transcribed Image Text:Consider a vector p = 3n +6b2 +9bz fixed in a spacecraft. At an instant in time the angular velocity of the spacecraft relative to Earth is i = 1.2b, +0.94bg+0.22b3 (in rad/s). What is the magnitude of the time derivative of the vector in the Earth reference frame. Note b1, b2, bz are unit vectors fixed in the spacecraft reference frame.
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