Device for optically guiding an autorotating missile
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United States of America Patent
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-
Oct 17, 1995
Grant Date -
N/A
app pub date -
Oct 28, 1981
filing date -
Nov 6, 1980
priority date (Note) -
Expired
status (Latency Note)
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Abstract
An optical guidance device comprises an entry lens of which the optical axis merges with the axis of rotation of the missile, a filiform infrared detector, sensitive to the infrared radiation of a target, is placed in the focal plane of the lens. The detector is intersected at least twice by circles centered on the axis of rotation of the missile. A circuit elaborates deviation information from the output signals from the detector. Steering means are provided for correcting the path of the missile from the deviation information.
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