Semi-automatic aircraft control system

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

73178T, 340407, 364434, G05D 112

Patent

active

040931595

ABSTRACT:
A flight control type system which provides a tactile readout to the hand of a pilot for directing elevator control during both approach to flare-out and departure maneuvers. For altitudes above flare-out, the system sums the instantaneous coefficient of lift signals of a lift transducer with a generated signal representing ideal coefficient of lift for approach to flare-out, i.e., a value of about 30% below stall. Error signals resulting from the summation are read out by the noted tactile device. Below flare altitude, an altitude responsive variation is summed with the signal representing ideal coefficient of lift to provide error signal readout.

REFERENCES:
patent: 2478967 (1949-08-01), Greene
patent: 2754505 (1956-07-01), Kenyon
patent: 2816724 (1957-12-01), Snodgrass
patent: 3418458 (1968-12-01), Majendie
patent: 3945593 (1976-03-01), Schanzer

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