Command guidance technique for line-of-sight missile

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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F41G 730

Patent

active

049679791

ABSTRACT:
A line of sight missile system wherein the missile includes a beacon and a eceiver, and the control station includes a telescope and a four-quadrant, polarizing encoder. The telescope is sighted on a target by the operator, the illumination from the beacon passes through the encoder and is reflected back to the receiver. The signal received by the receiver is processed within the missile and provides flight control instruction.

REFERENCES:
patent: 2404942 (1946-07-01), Bedford
patent: 2930894 (1960-03-01), Bozeman
patent: 3398918 (1968-08-01), Girault
patent: 3782667 (1974-01-01), Miller, Jr. et al.

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