Flight control system with tactile feedback

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244195, 244223, 364434, G05D 0100, B64C 1346

Patent

active

050625942

ABSTRACT:
A control system for an aircraft or other man-machine system wherein the usual visual feedback system is characterized and is optimally supplemented by a secondary feel oriented feedback arrangement in which input signals are derived from either of two supplementary feedback signal sources and the resulting algorithms characterized mathematically. The disclosure includes several exemplary arrangements of the feedback systems in which some of the input parameters are of selected value. Mathematical characterization of the feedback paths is used.

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patent: 4800721 (1989-01-01), Cemenska et al.
patent: 5016177 (1991-05-01), Lambregts

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