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Rocket demand analysis method and device, terminal equipment and medium

A demand analysis and terminal equipment technology, applied in the aerospace field, can solve problems such as difficulty in ensuring integrity and consistency, and achieve the effects of improving design efficiency and design quality, reducing understanding deviations, and reducing design costs

Pending Publication Date: 2022-03-22
AEROSPACE SCI & IND KET TECH CO LTD
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  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

In the traditional research and development of commercial space launch vehicles, the document-based system engineering method (Texted System Engineering, TES) is generally used to transmit design information in the form of documents. A lot of information is scattered in each document, and it is difficult to ensure completeness and consistency.

Method used

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  • Rocket demand analysis method and device, terminal equipment and medium
  • Rocket demand analysis method and device, terminal equipment and medium
  • Rocket demand analysis method and device, terminal equipment and medium

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Embodiment Construction

[0048] The embodiment of the present application provides a rocket requirement analysis method, which can improve rocket design efficiency and design quality, and reduce design cost.

[0049] The technical solution of the embodiment of the present application is to solve the above-mentioned technical problems. The general idea is as follows: obtain the user requirements of the launch vehicle, and store the user requirements in a structured form; refine and analyze the user requirements to Converting the user requirements into system requirements; establishing an association relationship between the user requirements and the system requirements; performing an allocation operation on the system requirements according to the pre-configured requirements baseline and the association relationship, so as to complete the Analysis and design of user needs.

[0050] In order to better understand the above-mentioned technical solution, the above-mentioned technical solution will be descr...

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Abstract

The invention discloses a rocket demand analysis method and device, terminal equipment and a medium, and the method comprises the steps: obtaining a user demand of a carrier rocket, and carrying out the entry storage of the user demand according to a structured form; extracting and analyzing the user demand so as to convert the user demand into a system demand; establishing an association relationship between the user demand and the system demand; and according to a pre-configured demand baseline and the association relationship, carrying out allocation operation on the system demand to complete analysis of the user demand. By adopting the method, demand analysis can be carried out on the carrier rocket, so that the understanding deviation of related parties on demands is reduced, the design efficiency and the design quality are improved, and the design cost is reduced.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a rocket demand analysis method, device, terminal equipment and medium. Background technique [0002] With the increase of commercial space missions and the intensification of competition, the high-frequency, low-cost, and fast-iterating market demand has put forward new requirements for the research and development of launch vehicles. [0003] Launch vehicle research and development is a complex system engineering involving many disciplines and a wide range of modules and systems. In the traditional research and development of commercial space launch vehicles, the document-based system engineering method (Texted System Engineering, TES) is generally used to transmit design information in the form of documents. A lot of information is scattered in each document, and it is difficult to ensure completeness and consistency. Model Based System Engineering (Model Based System Engi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/06G06Q10/04
CPCG06Q10/06315G06Q10/06313G06Q10/04
Inventor 熊双武朱佩婕闯三宇阮彩霞马道远杭万荣
Owner AEROSPACE SCI & IND KET TECH CO LTD
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