Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1978-10-25
1981-01-27
Blum, Theodore M.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 312, F41G 700, F42B 1502, G06F 1550
Patent
active
042470595
ABSTRACT:
An improved automatic missile tracking and guidance system wherein a laund missile is guided along a line-of-sight maintained by the operator with the target. The position of an infrared source disposed on the missile is detected and guidance signals generated in accordance therewith to control the flight of the missile along the line-of-sight. The infrared source or beacon disposed on the missile comprises an array of semiconductor light emitting diodes. The solid state characteristics of the light emitting diodes provide heretofore unobtainable reliability over existing beacons. The beacon may be used to produce a modulated, high frequency, rectangular waveform, incoherent emission offering performance improvements including virtual immunity to optical countermeasures.
REFERENCES:
patent: 3227882 (1966-01-01), Bissett et al.
patent: 3366346 (1968-01-01), McKnight et al.
patent: 4027837 (1977-06-01), Miller, Jr. et al.
patent: 4034949 (1977-07-01), Hoesterey et al.
patent: 4047678 (1977-09-01), Miller, Jr. et al.
Duke Jimmy R.
Fountain Walter F.
Kilbourn Dorwin L.
Mangus, Jr. Nicholas J.
Miller, Jr. Walter E.
Blum Theodore M.
Bush Freddie M.
Edelberg Nathan
Gibson Robert P.
The United States of America as represented by the Secretary of
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