Title :
Stability of a two-degree-of-freedom gyro with external feedback
Author_Institution :
Hughes Aircraft Company, Culver City, CA, USA
fDate :
7/1/1965 12:00:00 AM
Abstract :
The requirements for insuring the stability of the loop formed when external feedback is applied to a two-degree-of-freedom gyro are determined. The method of analysis also suggests the means for increasing the damping of the nutation of a precessible two-degree-of-freedom gyro when it is used in a free mode.
Keywords :
Gyroscopes; Stability; Construction; Damping; Feedback loop; Laplace equations; Missiles; Radar antennas; Radar tracking; Sensor systems; Stability; Torque;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1965.1098157
