Derive the translational and rotation kinematic equations for an aircraft using a 3-1-3 rotation sequence, rather...

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Derive the translational and rotation kinematic equations for an aircraft using a 3-1-3 rotation sequence, rather than the 3-2-1 rotation sequence provided in class. The angles used for these rotations are denoted 1, 0, and 4, respectively. For which angle, and at what magnitude of that angle, does the singularity occur? Recall that singularity refers to the orientation when the rotational kinematic equations are undefined. (13 points) Derive the translational and rotation kinematic equations for an aircraft using a 3-1-3 rotation sequence, rather than the 3-2-1 rotation sequence provided in class. The angles used for these rotations are denoted 1, 0, and 4, respectively. For which angle, and at what magnitude of that angle, does the singularity occur? Recall that singularity refers to the orientation when the rotational kinematic equations are undefined. (13 points)

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In aviation the standard Euler angle convention uses three successive rotations around the X Y and Zaxes commonly referred to as the 321 rotation sequ... View the full answer