Automatic approach pitch axis control system for aircraft

Details Automatic approach pitch axis control system for aircraft Automatic approach pitch axis control system for aircraft

1975-02-26

1976-11-30

Kunin, Stephen G.

Aeronautics and astronautics

Aircraft control

Automatic

23515022, G05D 112

Patent

active

039944557

ABSTRACT:
The invention relates to a system utilizing an exponential control law for glide slope capture. The capture maneuver from above or below the beam, is a function of decreasing glide slope beam error. The present autopilot approach coupler is an altitude rate command system which provides switchless signal processing during glide slope capture, and tracking.

REFERENCES:
patent: 2672334 (1954-03-01), Chenery
patent: 2987275 (1961-06-01), Moncrieff-Yeates et al.
patent: 3291421 (1966-12-01), Kramer et al.
patent: 3327973 (1967-06-01), Kramer et al.
patent: 3333795 (1967-08-01), Haltendorf et al.
patent: 3578269 (1971-05-01), Kramer et al.
patent: 3652835 (1972-03-01), Devlin et al.

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