Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1973-08-24
1976-03-16
Wilbur, Maynard R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
250203R, 250233, 250339, 250342, F11g 700, G01j 120
Patent
active
039441679
ABSTRACT:
A radiation sensor including an inner detector surrounded by an array of outer detectors is employed in radiation tracking apparatus which is capable of tracking a true target in a field of targets which may include a decoy or false target. The apparatus includes a color filter arrangement and a reticle which cooperates to produce pulses of long and short wavelength filtered infrared radiation upon the outer detectors of the sensor. The apparatus includes means for processing the signals produced by the outer and inner detector elements so as to discriminate between true and false targets and cause the tracking apparatus to track a true target.
REFERENCES:
patent: 2939962 (1960-06-01), Miller
patent: 3023661 (1962-03-01), McClusky et al.
patent: 3219826 (1965-11-01), Letaw, Jr.
patent: 3379891 (1968-04-01), Aroyan
patent: 3634689 (1972-01-01), Hachioji-shi et al.
patent: 3699345 (1972-10-01), Parkin
Figler Burton D.
Nussdorfer Theodore J.
Buczinski S. C.
Etlinger Louis
Sanders Associates Inc.
Seligman Richard I.
Wilbur Maynard R.
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