Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1962-10-12
1978-07-25
Engle, Samuel W.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
325 32, 178 22, 102214, F41G 714, F41G 900, F41G 700
Patent
active
041025210
ABSTRACT:
1. In a system for the coding of guidance signals which are produced at a control center and after their coding transmitted to a body to be guided, a control center consisting of a command generator for producing the guidance signals, a coding unit for coding the guidance signals, a storage stage feeding the coding unit, said storage stage being controlled by a time stage, and a transmitter for transmitting the coded guidance signals to the body to be guided for actuating conrol surfaces therein, furthermore a receiver for the transmitted guidance signals, which receiver is arranged in the body to be guided, a decoding unit coupled to the receiver, a servo mechanism of the control surfaces of the body coupled to the decoding unit, a storage stage coupled to feed the decoding unit, a time stage coupled to control the storage stage, and a code generator consisting of a noise generator and two gate circuits connected therewith, one of said gate circuits being connected to the storage stage of the control center and the other gate circuit being connected to the storage stage in the body to be guided, which last connection is provided with a releasable plug which disconnects said other gate circuit when the body to be guided is launched.
REFERENCES:
patent: 2530142 (1950-11-01), Atkins
patent: 3053478 (1962-09-01), Davenport et al.
Boelkow Entwicklungen KG
Engle Samuel W.
Webb Thomas H.
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