Inertial reference system for an aircraft

Details Inertial reference system for an aircraft Inertial reference system for an aircraft

2006-01-17

2006-01-17

Barefoot, Galen (Department: 3644)

Aeronautics and astronautics

Aircraft control

Automatic

C244S195000, C701S014000, C701S220000, C073S17800T

Reexamination Certificate

active

06986483

ABSTRACT:
An inertial reference system for an aircraft includes two accelerometers and a gyrometer. One accelerometer is located at a front portion of the aircraft, the other is located at a rear portion of the aircraft. The gyrometer is located at a center portion of the aircraft. The system also includes a control computer linked to the accelerometers and to the gyrometer. The center portion can include the aircraft's center of gravity.

REFERENCES:
patent: 2487793 (1949-11-01), Esval et al.
patent: 2985409 (1961-05-01), Atwood et al.
patent: 3549108 (1970-12-01), Smith
patent: 4171115 (1979-10-01), Osder
patent: 5072893 (1991-12-01), Chakravarty et al.
patent: 6669139 (2003-12-01), Kubica
patent: 2003/0205644 (2003-11-01), Najmabadi et al.

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