Variable sweep side force generator and roll control device

Aeronautics and astronautics – Aircraft control – Vertical fins

Patent

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Details

244 90R, 244 327, B64C 512

Patent

active

051508613

ABSTRACT:
In an airborne vehicle utilizing tail fins to provide directional control by use of the sideslip maneuver, a variably positionable side force generator airfoil that is positioned in response to the normal load factor of the vehicle to eliminate undesired roll caused by sideslip.

REFERENCES:
patent: 3826448 (1974-07-01), Burk, Jr.
patent: 4145017 (1979-03-01), Stiklorus
patent: 4247063 (1981-01-01), Jenkins
patent: 4296894 (1981-10-01), Schnabele et al.
patent: 4378922 (1983-04-01), Pierce
patent: 4601442 (1986-07-01), Friedel et al.
patent: 4739957 (1988-04-01), Vess et al.
patent: 4756253 (1988-07-01), Herring et al.

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