| 摘要 |
<p>PURPOSE:To obtain a missile, capable of preventing an interference between optical wave seeker and radio wave seeker and permitting transmission of radio wave and optical wave by mounting the optical wave seeker and the radio wave seeker non- coaxially. CONSTITUTION:An optical wave seeker 3 is mounted at the tip end of a missile and is protected from external field by a dome 1 while a radio wave seeker 9, observing and tracking the movement of a target by employing radio wave, is also mounted on the missile. The radio wave seeker 9 is mounted in the outer peripheral part of a fuselage and the missile is provided with a fore-wing configuration. A signal processing computer 7, inputting informations on the target from the optical wave seeker 3 and the radio wave seeker 9 and effecting an operation for guiding the missile to the target, is mounted in an apparatus mounting space in the fuselage, in which a sufficient room can be produced by mounting the radio wave seeker 9 in the outer peripheral space of the fuselage, so that the volume of the computer is expanded and the function of the same is improved. A mounting space, allotted to the mounting of other control devices, is also expanded. According to this constitution, an interfer ence between the optical wave seeker 3 and the radio wave seeker 9 is eliminated and functions of both seeker can be developed.</p> |
