Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1988-04-15
1989-08-29
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
F41G 732, F42B 1504
Patent
active
048609684
ABSTRACT:
Apparatus for optical fiber data link between two moving bodies remote controlled vehicle/missile such as ("RCV") and hereinafter launch platform includes fiber-wound bobbins having opposite winding directions on each body, interconnected with unwound, reinforced fiber sections, for streaming deployment from each bobbin through tensioning devices during relative separation movement between the two bodies. Image sensors and flight control mechanisms are operatively connected through a electric/optical I/O device to the fiber on the bobbin in the RCV, and data analysis/display devices and controller/command units are similarly interfaced with the fiber on the bobbin associated with the helicopter. The bobbin housing on the helicopter uses a shaped cavity and gimbal mount to provide free-streaming fiber deployment and pyrotechin or electro-mechanical separation device to discharge the bobbin and attached fiber after mission completion.
REFERENCES:
patent: 3613619 (1971-10-01), DeNobel
patent: 4185796 (1980-07-01), Riley
patent: 4573647 (1986-03-01), Laten et al.
patent: 4611771 (1986-04-01), Gibbons et al.
patent: 4770370 (1988-09-01), Pinson
Chaffee, C. David; "U.S. Military Programs Take Advantage of Fiber Optic Technology"; Laser Focus/Electro-Optics; 8/1986, pp. 80-83.
Jordan Charles T.
The Boeing Company
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