Automatic approach landing and go-around control system for airc

Communications: electrical – Selective – Having indication or alarm

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Details

73178T, 244188, G01C 2100, G01C 500, G08G 500

Patent

active

043192190

ABSTRACT:
A system for providing an aircraft pilot and/or autothrottle and go-around pitch axis control with information when a go-around should be initiated during an approach in response to either a hazardous flight status of the aircraft or to wind shear encounter by the aircraft. The present system utilizes a gain schedule control law based on the bug speed set by the pilot and on pilot go-around criteria to trigger a go-around signal for the pilot and/or the automatic control systems.

REFERENCES:
patent: 3496769 (1970-02-01), Vietor
patent: 3667293 (1972-06-01), Moore
patent: 3789661 (1974-02-01), Melsheimer
patent: 4021010 (1977-05-01), Bliss
patent: 4079905 (1978-03-01), Greene

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