A vector from the aircraft center of mass to a point on the wing is along the y-direction of the aircraft (body) reference frame and has a magnitude pf 7.5 m. At an instant in time, the orientation of the aircraft is given by ø = 13deg, 0 = 10deg, and p = 108deg. Calculate the z -component of the vector in the Earth frame (in m ).
A vector from the aircraft center of mass to a point on the wing is along the y-direction of the aircraft (body) reference frame and has a magnitude pf 7.5 m. At an instant in time, the orientation of the aircraft is given by ø = 13deg, 0 = 10deg, and p = 108deg. Calculate the z -component of the vector in the Earth frame (in m ).
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Transcribed Image Text:A vector from the aircraft center of mass to a point on the wing is
along the y-direction of the aircraft (body) reference frame and has a
magnitude pf 7.5 m. At an instant in time, the orientation of the
aircraft is given by ø = 13deg, 0 =
Calculate the z -component of the vector in the Earth frame (in m ).
10deg, and = 108deg.
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