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L10-4. Assume an aircraft has yaw = 7/12, pitch 0, = 7/12, and roll o1 = pi/6 with respect to the inertial framel Find the quaternion representation of the aircraft's orientation with respect to that same inertial frame. answer: q 0.9539+0.23796i+0.1585j +0.0915k could you please show me the process of how to obtain the quaternion.

L10-4. Assume an aircraft has yaw = 7/12, pitch 0, = 7/12, and roll o1 = pi/6 with respect to the inertial framel Find the quaternion representation of the aircraft's orientation with respect to that same inertial frame. answer: q 0.9539+0.23796i+0.1585j +0.0915k could you please show me the process of how to obtain the quaternion.

Advanced Engineering Mathematics
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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L10-4. Assume an aircraft has yaw = 7/12, pitch 01 = 7/12, and roll oi = pi/6 with respect to the inertial framel Find the quaternion representation of the aircraft's orientation with rèspect to that same inertial frame. %3D %3D answer: q = 0.9539+0.23796i+ 0.1585j + 0.0915k could you please show me the process of how to obtain the quaternion.
Transcribed Image Text:L10-4. Assume an aircraft has yaw = 7/12, pitch 01 = 7/12, and roll oi = pi/6 with respect to the inertial framel Find the quaternion representation of the aircraft's orientation with rèspect to that same inertial frame. %3D %3D answer: q = 0.9539+0.23796i+ 0.1585j + 0.0915k could you please show me the process of how to obtain the quaternion.
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