Aircraft crosswind control apparatus

Aeronautics and astronautics – Aircraft control – Automatic

Patent

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Details

244 91, 244103W, B64C 508, B64C 510, B64C 1316

Patent

active

057383316

ABSTRACT:
The present invention relates to a control system for an aircraft to compensate for crosswinds on landings. In one embodiment, the control system includes two mutually identical control surfaces having common end points, respectively; and an actuator to move completely the two mutually identical control surfaces, as needed to compensate for the crosswinds on landing.

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patent: 3912202 (1975-10-01), Jenkins
patent: 4457479 (1984-07-01), Daude
patent: 5069402 (1991-12-01), Wortman

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