Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1983-07-20
1985-09-10
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
343424, F41G 722
Patent
active
045401390
ABSTRACT:
A passive homing system for missiles is provided having at least three interferometric bases each comprising two electromagnetic antennae disposed on the missile. Said three interferometric bases have respective mid-perpendicular planes which are inclined two by two at 120.degree. with respect to each other.
REFERENCES:
patent: 3181813 (1965-05-01), Gulick, Jr. et al.
patent: 3740002 (1973-06-01), Schaefer
patent: 4108400 (1978-08-01), Groutage et al.
patent: 4204655 (1980-05-01), Gulick et al.
patent: 4264907 (1981-04-01), Durand, Jr. et al.
Levy Pierre
Robert Andre
Jordan Charles T.
Societe Anonyme de Telecommunications
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