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
053887840
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 armed decoy launched from a ship being attacked toward such missile, such decoy signals initially obscuring 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, and, when the decoy and guided missile are in proximity with one another, exploding a warhead on the decoy to destroy the guided missile.
REFERENCES:
patent: 3729150 (1973-04-01), Conger
patent: 3733604 (1973-05-01), Smith
patent: 3792477 (1974-02-01), Tomiyasu
patent: 3866225 (1975-02-01), Buck
patent: 3949955 (1976-04-01), Sykes et al.
patent: 3956729 (1976-05-01), Epstein et al.
patent: 4037227 (1977-07-01), Kline
patent: 4072949 (1978-02-01), Von Brunt
patent: 4164741 (1979-08-01), Schmidt
patent: 4216472 (1980-08-01), Albanese
Libby Wesley B.
Procaccino Roderic J.
Gangialosi Salvatore
Mofford Donald F.
Raytheon Company
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