Sensor device for a missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

35613907, 3561522, F41G 700, F41G 722

Patent

active

056695802

ABSTRACT:
Described is a sensor device (10) for a missile (16) having a matrix detector (12) and an electronic evaluation circuit connected thereto. A ray source (20) is stationarily arranged on the missile (16). Provided between the ray source (20) and the matrix detector (12) which is stationarily provided on the missile (16) is a gyro optical device (22) which is cardanically mounted in the missile (16). The sensor device may be employed to determine the roll position and roll rate of a missile (16).

REFERENCES:
patent: 3439170 (1969-04-01), Zagone et al.
patent: 4231533 (1980-11-01), Durig
patent: 4270044 (1981-05-01), Elwell, Jr.
patent: 4386848 (1983-06-01), Clendenin et al.
patent: 4701602 (1987-10-01), Schaefer et al.
patent: 4770482 (1988-09-01), Sweeney et al.
patent: 4796834 (1989-01-01), Ahlstrom
patent: 5088818 (1992-02-01), Nicholson
patent: 5456179 (1995-10-01), Lamelot

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