The gyro rotor is spinning at the constant rate p = 100 rev/min relative to the x-y-z
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The gyro rotor is spinning at the constant rate p = 100 rev/min relative to the x-y-z axes in the direction indicated. If the angle γ between the gimbal ring and horizontal X-Y plane is made to increase at the rate of 4 rad /sec and if the unit is forced to precess about the vertical at the constant rate N = 20 rev/min, calculate the angular momentum HO of the rotor when γ = 30°. The axial and transverse moments of inertia are Izz = 5(10−3) lb-ft-sec2 and Ixx = Iyy = 2.5(10−3) lb-ft-sec2.
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Related Book For
Engineering Mechanics Dynamics
ISBN: 9781118885840
8th Edition
Authors: James L. Meriam, L. G. Kraige, J. N. Bolton
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