Consider an aircraft at an orientation given by = 0.8 rad, 0 = 0.19 rad, o = 0.3 rad. The angles represent the rotations in a body 3-2-1 sequence. If a vector on the aircraft can be represented in the aircraft axis system as i = 5 b1. What is the y-component of the vector in the Earth/inertial axis system?
Consider an aircraft at an orientation given by = 0.8 rad, 0 = 0.19 rad, o = 0.3 rad. The angles represent the rotations in a body 3-2-1 sequence. If a vector on the aircraft can be represented in the aircraft axis system as i = 5 b1. What is the y-component of the vector in the Earth/inertial axis system?
Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
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Transcribed Image Text:Consider an aircraft at an orientation given by b = 0.8
rad, 0 = 0.19 rad, o = 0.3 rad. The angles represent the
rotations in a body 3-2-1 sequence. If a vector on the
aircraft can be represented in the aircraft axis system as
i = 5 b1. What is the y-component of the vector in the
Earth/inertial axis system?
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