Aircraft landing control system

Details Aircraft landing control system Aircraft landing control system

1980-02-22

1982-11-02

Gruber, Felix D.

Boots, shoes, and leggings

244183, 244187, G05D 112, G06G 770, B64C 1318

Patent

active

043576613

ABSTRACT:
Upon aircraft landing approach, flare path command signals of altitude, vertical velocity and vertical acceleration are generated as functions of aircraft position and velocity with respect to the ground. The command signals are compared with corresponding actual values to generate error signals which are used to control the flight path.

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patent: 3523663 (1970-08-01), Doniger et al.
patent: 3523664 (1970-08-01), Doniger et al.
patent: 3545703 (1970-12-01), Montvale
patent: 3578269 (1971-05-01), Kramer et al.
patent: 3665465 (1972-05-01), Miller
patent: 3666929 (1972-05-01), Menn
patent: 3705306 (1972-12-01), Lydon et al.
patent: 4141522 (1979-02-01), Lambregts

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