NASA NTRS ยท 19860000111
Blending Gyro Signals To Improve Control Stability
Abstract
Interference by structural vibrations reduced by adding signals from spatially separated gyros. Technique involves blending signals from rate gyroscopes located at different parts of structure to obtain composite signal that more nearly represents rotation of entire structure. Aircraft vibrations perpendicular to pitch axis contribute to rotations sensed by pitch-rate gyros. Proper blending of signals from gyros suppress contribution of dominant vibrational mode. Most likely applications of concept are flight-control systems for aircraft.
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J. F. L. Lee. 1986-05-01. Blending Gyro Signals To Improve Control Stability. https://ntrs.nasa.gov/citations/19860000111
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