3814912 is referenced by 34 patents and cites 4 patents.

A system for deriving signals proportional to horizontal and vertical wind gust level each as the difference between an atmospheric measurement and an inertial reference and, by a threshold sensitive signal translator responsive only to negative ones of the derived signals, to subtract gust bias signals from the system angle-of-attack reference to compensate for those gust components which tend to reduce lift.

Title
Gust compensation for angle-of-attack reference aircraft speed control system
Application Number
05/321,100
Publication Number
3814912
Application Date
January 4, 1973
Publication Date
June 4, 1974
Inventor
Klein James A
Schuldt Jr Theodore J
Manke Girard M
Assignee
Collins Radio Company
IPC
G06g 07/70
B64c 13/16
G05D 01/00
G05D 01/06
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