FIELD: optical instrumentation.
SUBSTANCE: invention relates to the field of optical instrumentation and relates to a method of optoelectronic guidance and remote detonation of a guided missile. When implementing the method, the object is periodically illuminated with frequencies f1 and f2 by laser radiation at the first and second wavelengths in mismatched time intervals. The reflected radiation beams are spectrally filtered, defocused and recorded by a photodetector. Next, object registration signals and object angular mismatch signals are generated by their sum-difference processing, the distance to the object is measured, the remote detonation signal is generated when registering a given sequence of object detection signals and at a distance to the object not higher than the specified one. The formation of laser radiation and its reception is carried out inside temporary gates, the radiation pattern at the second wavelength is formed in the form of a hollow conical surface.
EFFECT: increasing in the accuracy of pointing and triggering the fuse while increasing the angular field of view.
5 cl, 7 dwg
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Authors
Dates
2023-03-07—Published
2022-03-18—Filed