Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1995-11-15
1997-09-23
Carone, Michael J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
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).
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patent: 4796834 (1989-01-01), Ahlstrom
patent: 5088818 (1992-02-01), Nicholson
patent: 5456179 (1995-10-01), Lamelot
Carone Michael J.
Diehl GmbH & Co.
Montgomery Christopher K.
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