A compact miniaturized integrated missile controller

Abstract

The invention discloses a compact type small integration type guided missile controller. The compact type small integration type guided missile controller comprises a shell, a navigation circuit board, a GPS signal board, a computer circuit board, a power circuit board, a steering engine power amplifier circuit, a communication protocol circuit board and a metallic shield board, wherein the navigation circuit board, the GPS signal board, the computer circuit board, the power circuit board, the steering engine power amplifier circuit, the communication protocol circuit board and the metallic shield board are jointly arranged in the shell; the shell comprises a shell body and a connecting rod, the shell body comprises a bottom cover, a circuit board support I, a circuit board support II, a circuit board support III and an upper cover, the bottom cover is divided into two independent spaces through a first partition board, one independent space is horizontally provided with the navigationcircuit board, the other independent space is horizontally provided with the GPS signal board and the metallic shield board, the upper cover is divided into two independent spaces through a second partition board, one independent space is provided with the communication protocol circuit board, and the other independent space is provided with an external electrical connector. The compact type small integration type guided missile controller has the advantages of being small in size, simple in structure, convenient to mount, good in cable layout and high in system anti-electromagnetic interference capacity and can be popularized and applied to a small missile weapon system.

Description

technical field [0001] The invention belongs to the field of airborne weapon control systems, and more specifically relates to a missile controller. Background technique [0002] With the development of precision guided weapons, higher requirements are put forward for their miniaturization, high damage and precision strike. Each control unit of a missile in the traditional form is a stand-alone independent of each other; the independence of the system leads to the bulky and heavy weight of the entire aircraft control system, and each stand-alone needs to be adjusted after leaving the factory, especially for miniaturized missiles. The installation structure is complicated, and the layout of the communication cables between the stand-alone and the stand-alone is difficult, which reduces the payload. Contents of the invention [0003] Aiming at the above defects or improvement needs of the prior art, the present invention provides a compact and miniaturized integrated missil...

AI Technical Summary

Problems solved by technology

Each control unit of a missile in the traditional form is a stand-alone independent of each other; the independence of the system leads to the bulky and heavy weight of the entire aircraft control system, and each stand-alone needs to be adjusted after leaving the factory, especially for miniaturized missiles. The installation structure is complicated, and the layout of the communication cables between the stand-alone and the stand-alone is difficult, which reduces the payload

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