Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1984-11-28
1986-07-08
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
102476, F41G 726, F42B 1310
Patent
active
045988846
ABSTRACT:
A gimbal-less infrared (IR) target sensor for mounting in an IR transmissive nose cone of a guided missile comprises a fixed, concave, primary mirror mounted coaxially in the base of the nose cone; a fixed, convex, secondary mirror mounted at the focus of the primary mirror; and a plurality of IR sensing units having IR transmissive elements located around the periphery of the primary mirror. A shaped-charge is located aft of the primary mirror. The IR-transmissive elements incorporate IR-conductive fiber optics to transmit the IR signal to detectors aft of the shaped-charge for detection, processing, and missile guidance.
REFERENCES:
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patent: 2457393 (1948-12-01), Muffly
patent: 2969018 (1961-01-01), Erst et al.
patent: 3021096 (1962-02-01), DeMott
patent: 3072055 (1963-01-01), Ross
patent: 3782667 (1974-01-01), Miller, Jr. et al.
patent: 4106726 (1978-08-01), Emmons et al.
patent: 4131248 (1978-12-01), Bergland
General Dynamics Pomona Division
Johnson Edward B.
Jordan Charles T.
Martin Neil F.
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