Electronic foot controls

Aeronautics and astronautics – Aircraft control – Pilot operated

Patent

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Details

244236, 200 865, 338153, 338128, 114144R, 440 7, B64C 1304

Patent

active

051218895

ABSTRACT:
A six-way foot control device has a toe portion pivotally mounted to a heel portion so that two directions of angular toe displacement may be realized about a neutral position. The heel portion is itself pivotally mounted to permit two directions of sideways angular displacement about a corresponding second neutral point. Finally, the foot control is slidably mounted to permit two directions of linear displacement about a third neutral point. Each direction of displacement is detected by a transducer and may control another function of an aircraft or vehicle.

REFERENCES:
patent: 2379774 (1945-07-01), Wyer
patent: 2460494 (1949-02-01), Esienberg et al.
patent: 2986953 (1961-06-01), Armand et al.
patent: 2992797 (1961-07-01), Visser
patent: 3833782 (1974-09-01), Bartel
patent: 4120387 (1978-10-01), Otteblad et al.
patent: 4237752 (1980-12-01), Hildebrecht
patent: 4614900 (1986-09-01), Young

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