Missile steering system using a segmented target detector and st

Details Missile steering system using a segmented target detector and st Missile steering system using a segmented target detector and st

1967-11-27

1983-04-26

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 722, F42B 1502

Patent

active

043810900

ABSTRACT:
A missile control and guidance system employing a combination of generally ertically disposed ailerons and generally horizontally disposed elevators. In order to make a horizontal turn, a combination of aileron and elevator deflections is used, to cause the missile to make a "blanked" turn. The ailerons and elevators are controlled by servos activated by a logic circuit. The logic circuit is connected to a segmented target detector. The missile will maneuver depending on which of the segments of the detector "sees" a target.

REFERENCES:
patent: 2403387 (1946-07-01), McLennan
patent: 2520433 (1950-08-01), Robinson
patent: 2588382 (1952-03-01), Hammond
patent: 2994270 (1961-08-01), Hull
patent: 3128061 (1964-04-01), Chew
patent: 3233848 (1966-02-01), Byrne

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