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Considering I know the accelerations [ax, ay, az] and angular rates [p, q, r] at the center of gravity (cg) of an airplane. How can I calculate the accelerations and angular rates at the pilot's position (p).
I have information about the distance between the cg and the pilot's position which could be characterized by a 3 dimensional vector (R).
Any help would be appreciated.
Best regards to all.
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