Aircraft guidance system for take off or go-around during severe

Details Aircraft guidance system for take off or go-around during severe Aircraft guidance system for take off or go-around during severe

1983-03-09

1986-09-02

Chin, Gary

Boots, shoes, and leggings

364434, 364427, 244181, 244182, 73178T, G05D 108

Patent

active

046099875

ABSTRACT:
A system which provides an increased minimum aircraft pitch attitude during take-off or go-around operations in the event that an unsafe wind shear condition is encountered. A control signal from a wind shear warning system, indicative of a dangerous wind shear condition, is fed to a switching device which controls the velocity command signal to the flight director pitch control. This switching device, in response to the wind shear signal, changes the velocity command to a lower predetermined value, such that the attitude of the aircraft is automatically increased to handle the wind shear encounter.

REFERENCES:
patent: 3892374 (1975-07-01), Lambregts
patent: 3955071 (1976-05-01), Lambregts
patent: 3981442 (1976-09-01), Smith
patent: 4189118 (1980-02-01), Peter-Contesse et al.
patent: 4189119 (1980-02-01), Peter-Contesse et al.
patent: 4212444 (1980-07-01), Stephan
patent: 4319219 (1982-03-01), Rein-Weston
patent: 4347572 (1982-08-01), Berwick, Jr. et al.
patent: 4422147 (1983-12-01), Hanke

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