Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1978-08-15
1980-12-30
Blum, Theodore M.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 319, 343 18E, F41G 700, F42B 1502, G06F 1550
Patent
active
042418895
ABSTRACT:
A method and device is disclosed for increasing the hit probability of guided missiles exposed to jamming by double or multiple targets. In particular, the missiles are guided by the proportional navigation principle and have a follow-up target-seeking head. With the addition of a plurality of tracking filters, means for performing data analysis and means for performing data control to a conventional missile guidance system, signals from the target-seeking head or the missile may be analyzed to provide recognition of double or multiple target situations. Once recognition of the double or multiple target situation is made, the flow of data for controlling the guidance and target-seeking head follow is corrected to keep the missile permanently on the target.
REFERENCES:
patent: 4160974 (1979-07-01), Stavis
Lenz Rudiger
Schwellinger Ulrich
Blum Theodore M.
Messerschmitt-Bolkow-Blohm GmbH
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