Launch control device and method suitable for dual-missile launch

Abstract

The invention provides a launch control device and method suitable for dual-missile launch. The launch control device comprises: a first transceiver module, a second transceiver module, a DSP processor module, a gating module, and an upper computer module; the first transceiver module is connected with the DSP processor module; the upper computer module and the DSP processor module are connected in series through the second transceiver module; the gating module is connected in series with the DSP processor module and the upper computer module, respectively, and the gating module outputs the information of any one information channel or any number of information channels to the upper computer module according to a gating instruction and real-time information output by the upper computer module. The launch control device provided by the invention is reasonable in design and is convenient to use, provides an information channel gating function, especially a video gating function, in a missile launch process, which is beneficial to controlling the missile launch in a missile weapon system with an optical imaging guide device.

Description

technical field [0001] The invention relates to the field of automatic control, in particular to a launch control device and method suitable for launching dual-engine missiles, especially a dual-engine missile launch control equipment with a video gating function. Background technique [0002] Missile launch control equipment is an important part of the missile weapon system. It receives instructions from the host computer and performs various operations related to missile launch. Missile launch control equipment generally includes communication circuits, missile power-up circuits and missile launch circuits. Typically, missiles only have an electrical interface to launch and control equipment. In the missile weapon system with optical imaging guidance equipment, the missile needs to upload the video signal to the host computer through the launch control equipment, and the multi-launch missile launch control equipment needs to have the function of video channel selection. ...

AI Technical Summary

Problems solved by technology

This patent has no information channel gating function, especially video gating function; it is not conducive to the control of missile launch in missile weapon systems with optical imaging guidance equipment

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