Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1979-08-10
1995-02-14
Gangialosi, Salvatore
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
F41G 700
Patent
active
053887832
ABSTRACT:
A method of interdicting a guided missile equipped with an active radar-controlled guidance system is shown to include generating decoy signals in a transponder on an decoy launched from a ship being attacked, such decoy signals being formed by amplifying echo signals from the ship to cause the apparent position of the ship (as measured by the active radar-controlled guidance system) to differ from the actual position of the ship so that the guided missile ultimately is caused to miss the ship.
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patent: 3618096 (1971-11-01), Schoneborn
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patent: 3891989 (1975-06-01), Barney et al.
patent: 4117484 (1978-09-01), Shizume
patent: 4159478 (1979-06-01), Jaklitsch et al.
Gangialosi Salvatore
Mofford Donald F.
Raytheon Company
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