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A target launch control system

A technology of measurement, launch and control system and test system, which is applied to targets, moving targets, offensive equipment, etc., can solve the problems of long launch preparation time, large number of stand-alone equipment, and complicated shooting range operations, so as to shorten the launch preparation time and simplify the connection. Complexity, the effect of simplifying connection operations

Active Publication Date: 2021-09-03
HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0003] The existing target launch and control system mainly includes a remote control module and an execution module. These two parts are connected by cables. The remote control module is responsible for human-computer interaction and conveys combat commands. The execution module receives combat commands through the connection cable and executes target targeting. In order to ensure the reliability and controllability of the command, the signal volume on the current connection cable is very large, which also makes the cable bulky and complicated.
Therefore, most of the current target launch and control systems have problems such as large number of stand-alone equipment, complex systems, high costs, complex range operations, long launch preparation time, and difficulty in quickly expanding functions to achieve intensive target supply.

Method used

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Embodiment Construction

[0025] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0026] In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other. The present invention will be further described in detail below in combination with specific embodiments.

[0027] figure 1 It is a schematic diagram of a target launch control system according to an embodiment of the present invention. Such as figure 1 As shown, a target launch control system includes a remote control module, a launch control test system module and a power supply modu...

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Abstract

The invention discloses a target launch control system. The system includes a remote control module, a launch control test system module and a power supply module. The remote control module is respectively connected to the launch control test system module and the power supply module. According to the first command, the second command, the third command and the launch command of the remote control module, the system module treats the launched target missiles respectively, collects the corresponding test results and sends them to the remote control module, and the remote control module respectively receives the data collected by the launch control test system module. The test results of each stage of the test are judged whether the test results of each test stage are qualified. After passing the test, the corresponding instructions of each stage are sent to the launch control test system module. After all the test results are qualified, the launch command is sent to the launch control test system module. The system module sends an ignition command to the target missile to be launched to realize the launch of the target missile to be launched, thereby simplifying the preparation work before the launch of the target missile and reducing the connection cables at the remote end.

Description

technical field [0001] The invention belongs to the field of missile control, and in particular relates to a target launch control system. Background technique [0002] The main function of the target missile is to provide the missile with a target as a target in the test to verify the performance of the missile. The simulated docking test of the target missile is a test process that must be practiced before the launch test, and is an important part of the target missile launch control system. Among them, the main function of the ground measurement, launch and control system is to conduct a comprehensive inspection and confirm the functions and parameters of the aircraft before launch, eliminate technical risks in advance, and ensure the flight test mission. [0003] The existing target launch and control system mainly includes a remote control module and an execution module. These two parts are connected by cables. The remote control module is responsible for human-compute...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F41J9/08
CPCF41J9/08
Inventor 田玉琴屈汝祥何昱陶婷林添福胡国飞
Owner HUBEI SANJIANG AEROSPACE HONGFENG CONTROL
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