Intelligent launch control testing system for rocket

A technology of measurement and control system and testing system, which is applied in the direction of projectiles, measuring devices, instruments, etc., can solve the problems that there is no precedent for the application of intelligent measurement and control system, and achieve the reduction of labor costs, saving of human resources, and system Effect of Reliability Improvement

Inactive Publication Date: 2019-11-05
BEIJING ONESPACE TECH CO LTD +4
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the rocket test and launch control system, the traditional test and launch control system is currently used, and there is no precedent for the application of the intelligent test and launch control system

Method used

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  • Intelligent launch control testing system for rocket
  • Intelligent launch control testing system for rocket
  • Intelligent launch control testing system for rocket

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Embodiment Construction

[0021] 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 related inventions, rather than to limit the invention. It should also be noted that, for the convenience of description, only the parts related to the invention are shown in the drawings.

[0022] It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0023] Such as image 3 As shown, a rocket intelligent test and launch control system includes a test and launch control system 1, a test system 2, a data system 3 and an interpretation system 4; the test and launch control system 1 is connected to the test system 2, and the test sys...

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Abstract

The invention discloses an intelligent launch control testing system for a rocket. The intelligent launch control testing system comprises a launch control testing system body, a test system, a data system and an interpretation system; the launch control testing system body is connected with the test system, the test system is connected with the data system, and the data system is connected with the interpretation system. According to the intelligent launch control testing system for the rocket, a flow process of intelligent launch control testing is provided, intelligent automatic testing, automatic monitoring and automatic judgement are different from a traditional launch control testing system needing multisystem manual monitoring and interpretation, reduction of a complex test flow process is facilitated, lots of manpower resources are saved, and the human cost is reduced; intelligent operation is beneficial for reducing careless omissions caused by human factors, the system reliability is greatly improved, and the work efficiency is improved.

Description

technical field [0001] The invention relates to the field of rocket measurement and launch control systems, in particular to an intelligent rocket measurement and launch control system. Background technique [0002] The role of the test and launch control system (referred to as the test launch control system) includes two aspects: one is testing. Through testing, potential problems in various systems or stand-alone equipment on the arrow are found, and the problems are exposed in advance before take-off, so as to ensure subsequent The safety and reliability of the flight test; the second is the launch control, which is used to complete a series of tasks related to the launch, such as completing the binding of elements and programming of the software, binding the flight program, determining the initial state, igniting on time, and implementing emergency shutdown in case of failure Wait. Therefore, the success or failure of a flight, the measurement launch control system will...

Claims

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Application Information

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IPC IPC(8): G01D21/02F42B15/01
CPCF42B15/01G01D21/02
Inventor 戴龙鹏
Owner BEIJING ONESPACE TECH CO LTD
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