Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1984-11-07
1986-10-28
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 726
Patent
active
046194215
ABSTRACT:
A sensor arrangement in a tracking or search head which is equipped with a two-axis cardan frame system for the movements of a sensor relative to the search head. In the sensor arrangement of the above constructive type, the cardan frame system and the sensor which is axially offset ahead thereof, are supported by paired spherical surfaces which are passed through by a spine passageway and are interconnected through the intermediary of a parallelogram linkage.
REFERENCES:
patent: 4085910 (1978-04-01), Baker et al.
patent: 4339097 (1982-07-01), Kordulla et al.
patent: 4558325 (1985-12-01), Strom
Diehl GmbH & Co.
Jordan Charles T.
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