Weapon guidance system (AER-716B)

Details Weapon guidance system (AER-716B) Weapon guidance system (AER-716B)

1986-02-03

1995-01-10

Cangialosi, Salvatore

Aeronautics and astronautics

Missile stabilization or trajectory control

Remote control

244 313, 244 314, F42B 1500

Patent

active

053799666

ABSTRACT:
A missile guidance system including a sensor for detecting the position of a target and for detecting the position of a missile. A fire control processor is provided that computes a trajectory for the missile to the target and is connected to the sensor to determine any variations between the actual missile position from a computed trajectory missile position. A transmitter connected to this guidance computer then provides guidance information to the missile. The guidance information includes the missile position relative to the target and enables a processor on board the missile to recompute a new trajectory to the target. This guidance information is transmitted as a single pulse during a predetermined time interval as a periodic update to the missile.

REFERENCES:
patent: 3028119 (1962-04-01), Coble
patent: 3073550 (1963-01-01), Young
patent: 3820742 (1974-06-01), Watkins
patent: 4003659 (1977-01-01), Conard et al.
patent: 4008869 (1977-02-01), Weiss
patent: 4097007 (1978-06-01), Fagan et al.
patent: 4111385 (1978-09-01), Allen
patent: 4179088 (1979-12-01), French
patent: 4516743 (1985-05-01), Sweeney et al.

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