System for guiding the end phase of guided autonomous missiles

Details System for guiding the end phase of guided autonomous missiles System for guiding the end phase of guided autonomous missiles

1997-12-15

1999-08-03

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

102401, 102427, F41G 700, F42B 2200, F42C 2202

Patent

active

059314109

ABSTRACT:
A system for guiding the end phase of guided autonomous missiles consists of a marker unit having a sensor, a signature transmitter and a device for attachment to the target, as well as a cooperating direction finder in the guided missile.

REFERENCES:
patent: 4281809 (1981-08-01), Oglesby et al.
patent: 4375168 (1983-03-01), Swenson et al.
patent: 4540139 (1985-09-01), Levy et al.
patent: 4867034 (1989-09-01), Trosky et al.
patent: 4997144 (1991-03-01), Wolff et al.
patent: 5118050 (1992-06-01), Arnold et al.
patent: 5131602 (1992-07-01), Linick
patent: 5458041 (1995-10-01), Sun et al.

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