Calculate body components of aircraft’s angular velocity

Reference no: EM13250143

An aircraft has constant roll and pitch angles of ?=10 degrees and ?=10 degrees, and a constant yaw rate of ?'=6 deg/sec. Calculate the body components of the aircraft’s angular velocity: p, q, and r. Convert these components to calculate the angular velocity in Earth-fixed components.

Please provide clear explination and solution.

Reference no: EM13250143

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