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The aircraft velocity vector expressed in the Earth-fixed reference frame is V = UI + VJ + WK = 6.66371 + 289.1164J-407.8815K (ft/sec) and
The aircraft velocity vector expressed in the Earth-fixed reference frame is V = UI + VJ + WK = 6.66371 + 289.1164J-407.8815K (ft/sec) and in the aircraft fixed body reference frame it is given by V = ui + vj+wk = 497.7939i + 17.4497j + 43.5513k (ft/sec) Find the attitude of the aircraft in terms of its Euler angles (Y, 0, 0). Is your answer unique?
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College Physics
Authors: Jerry D. Wilson, Anthony J. Buffa, Bo Lou
7th edition
9780321571113, 321601831, 978-0321601834
