Method and apparatus for determining when a glide slope signal e

Aeronautics and astronautics – Aircraft control – Automatic

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343108R, 364429, G05D 112

Patent

active

041643402

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: 2439044 (1968-04-01), Ferrill, Jr.
patent: 3335980 (1967-08-01), Doniger et al.
patent: 3489378 (1970-01-01), Watson et al.
patent: 3596855 (1971-08-01), Barling
patent: 3994455 (1976-11-01), Simpson

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