Shear detection and compensation circuit for aircraft throttle c

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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73178R, 340 27SS, 364440, G05D 108

Patent

active

041891180

ABSTRACT:
A system for processing signals representative of airspeed error and inertial longitudinal acceleration in first and second channels, respectively, and providing cancellation of the turbulence-induced components of the respective signals. Shear detection and compensation circuits are provided in the system for reducing speed wandering in moderate and heavy turbulence. A circuit processing the signal .DELTA.V from the shear detector circuit is utilized to provide a gust bias signal input in the system.

REFERENCES:
patent: 3691356 (1972-09-01), Miller
patent: 3892374 (1975-07-01), Lambregts

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