Question: The system in Figure 1 is a simple model for a rate gyro, which uses gyroscopic effects to measure yaw rates. The rotor, which spins

The system in Figure 1 is a simple model for a rate gyro, which uses gyroscopic effects to
measure yaw rates. The rotor, which spins at a constant rate \phi _(o)^() about the body-fixed 3 axis,
reacts to \psi _(o)^(), the yaw rate of the frame, by a nutation deflection, \theta . For this problem, you may
assume the following: the spring k limits \theta to small angles, \psi _(o)^() is constant and purely vertical,
and the damper provides a torque of b\theta _(o)^() that resists rotation about the 1 axis. In this problem,
you will make use of the axis of symmetry (of the suspended body) and define two different
vec(\omega )'s, one for the body and one for the 1-2-3 axes (which will be different).
A\theta it is given by,
I_(1)\theta ^()+b\theta ^()+[(I_(1)-I_(3))\psi _(o)^()^(2)+kL^(2)]\theta -I_(3)\psi _(o)^()\phi _(o)^()=0
Note: this is a common equation that you would study in vibration class.
B\theta and
the yaw rate \psi _(o)^()\theta is constantkL^(2)(I_(1)-I_(3))\psi _(o)^()^(2), that is, the spring is very stiff, that there is a linear
relationship between \theta and \psi _(o)^().
Figure 1.
The system in Figure 1 is a simple model for a

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