Gust bias signal-generating circuit for aircraft throttle contro

Details Gust bias signal-generating circuit for aircraft throttle contro Gust bias signal-generating circuit for aircraft throttle contro

1977-11-22

1980-07-15

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft control

Automatic

73178R, 244188, 340 27SS, 364431, G05D 108

Patent

active

042124441

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: 3662976 (1972-05-01), Gesler
patent: 3814912 (1974-06-01), Manke et al.
patent: 3955071 (1976-05-01), Lambreets

Affiliated with

Also associated with

Rating

Gust bias signal-generating circuit for aircraft throttle contro does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gust bias signal-generating circuit for aircraft throttle contro, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gust bias signal-generating circuit for aircraft throttle contro will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-460570