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Carrier rocket environmental suitability analysis method and system, terminal and medium

A technology of environmental adaptability and launch vehicles, which is applied in special data processing applications, instruments, electrical digital data processing, etc., and can solve problems such as over-reliance on environmental tests

Pending Publication Date: 2021-01-05
CHINA ACAD OF LAUNCH VEHICLE TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The embodiment of the present application provides a launch vehicle environmental adaptability analysis method, system, terminal and medium, which can solve the problem of excessive dependence on environmental tests in environmental adaptability assessment, avoid repeated ground tests, and save development costs

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  • Carrier rocket environmental suitability analysis method and system, terminal and medium
  • Carrier rocket environmental suitability analysis method and system, terminal and medium
  • Carrier rocket environmental suitability analysis method and system, terminal and medium

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Embodiment Construction

[0024] In order to make the technical solutions and advantages in the embodiments of the present application clearer, the exemplary embodiments of the present application will be further described in detail below in conjunction with the accompanying drawings. Apparently, the described embodiments are only part of the embodiments of the present application, and Not an exhaustive list of all embodiments. It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other.

[0025] The environmental adaptability risk identification and control of the launch vehicle is related to the success or failure of the mission, which has a significant impact on the launch vehicle's occupation of the market. In related technologies, the environmental adaptability analysis method of launch vehicles is based on the "design-analysis-verification" single-chain analysis of each product, which is highly...

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Abstract

The embodiment of the invention provides a carrier rocket environment adaptability analysis method and system, a terminal and a medium, and relates to a carrier rocket technology. The method comprisesthe following steps: carrying out environmental adaptability weak link identification based on a carrier rocket full life cycle time sequence; when an environment adaptability weak link exists, carrying out analog analysis on the environment adaptability weak link based on data driving, and determining whether environment test verification is carried out according to the result of analog analysis; and when it is determined that environmental test verification is carried out and a test result satisfies a corresponding condition, determining that the verification is passed, and releasing an environmental adaptability weak link passing the verification. According to the invention, the problem that environmental adaptability evaluation excessively depends on environmental tests can be solved,repetition of ground tests is avoided, and development cost is saved.

Description

technical field [0001] The present application relates to launch vehicle technology, in particular to a launch vehicle environmental adaptability analysis method, system, terminal and medium. Background technique [0002] Environmental adaptability risk identification and control of commercial launch vehicles is related to the success or failure of the mission, which has a significant impact on the launch vehicle's occupation of the market. [0003] In related technologies, the environmental adaptability analysis method of launch vehicles is based on the "design-analysis-verification" single-chain analysis of each product, which is highly dependent on environmental tests: the environmental adaptability assessment of traditional models must be carried out in various Force, heat, electromagnetic, and natural environment tests can lead to conclusions. If design changes occur, repeated test verification will be carried out, resulting in a large number of over-test phenomena, whi...

Claims

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Application Information

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IPC IPC(8): G06F30/15G06F30/20G06F119/02
CPCG06F30/15G06F30/20G06F2119/02
Inventor 张子骏李炳蔚王尧孙静怡丁晨余慕春龚旻张东南宫自军牛智玲马靓徐子健年永尚吕薇许奇
Owner CHINA ACAD OF LAUNCH VEHICLE TECH
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