When simulating the motion of a spinning projectile, it turns out to be computationally advantageous to...

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When simulating the motion of a spinning projectile, it turns out to be computationally advantageous to select non-rolling frame measure numbers of the projectile mass center velocity and angular velocity for use in the equations of motion. Assume standard Euler angles using the aerospace rotation sequence (3-2-1) are used to define orientation. Reference frame N is the frame just before roll rotation (final rotation by roll angle 6). Let angular velocity be given by @Â/1 = pỈn + đỈn + řĶn. Solve for the rotational kinematic differential equations relating angular velocity measure numbers p, q, and the derivatives of Euler angles, è y. Make sure to isolate the Euler angle derivatives on the left-hand-side of the equation. 9 When simulating the motion of a spinning projectile, it turns out to be computationally advantageous to select non-rolling frame measure numbers of the projectile mass center velocity and angular velocity for use in the equations of motion. Assume standard Euler angles using the aerospace rotation sequence (3-2-1) are used to define orientation. Reference frame N is the frame just before roll rotation (final rotation by roll angle 6). Let angular velocity be given by @Â/1 = pỈn + đỈn + řĶn. Solve for the rotational kinematic differential equations relating angular velocity measure numbers p, q, and the derivatives of Euler angles, è y. Make sure to isolate the Euler angle derivatives on the left-hand-side of the equation. 9

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Answer The rotational given Scenario Scenario can W B1 Let 0 V b... View the full answer