A gyroscope with a single degree of freedom isshown in Figure P3.27. Gyroscopes sense the angularmotion of a system and are used in automatic flightcontrol systems. The gimbal moves about the outputaxis OB. The input is measured around the input axisOA. The equation of motion about the output axisis obtained by equating the rate of change of angular momentum to the sum of torques. Obtain a statespace representation of the gyro system.
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