Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1998-01-02
2000-06-20
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 726
Patent
active
060767650
ABSTRACT:
A reticle for a guidance seeker for spinning projectiles comprises a substrate; a pattern of a plurality of alternating light modulating structures, such as opaque and light transmitting, or light absorbing and light reflecting areas on the substrate such that an image of a target moving on the substrate will generate a plurality of pulses corresponding to the number of lines crossed by the image, the number of pulses increasing as the image moves outwardly from the center of the reticle; and a distinguishable, unambiguous, and singly periodic feature of the pattern, which is readily detectable every time the target image moves circumferentially, completing a full circle around the center of the reticle.
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Buckley Denise
Jordan Charles T.
Primex Technologies Inc.
Rosenblatt Gregory S.
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