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Satellite task demand configuration method and system

A configuration method and task technology, applied in the aerospace field, can solve problems such as high manpower dependence, long time consumption, and low processing efficiency, and achieve the goal of improving autonomous operation capabilities, improving efficiency and information support capabilities, and enhancing the level of intelligent management and control Effect

Inactive Publication Date: 2021-07-16
NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the decision-making process of task requirements, there are problems such as low processing efficiency, long time-consuming, high dependence on manpower, low level of intelligence, and lack of human resources.

Method used

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  • Satellite task demand configuration method and system
  • Satellite task demand configuration method and system
  • Satellite task demand configuration method and system

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Embodiment Construction

[0029] Attached to the following Figures 1 to 3 This embodiment will be described.

[0030] The specific implementation steps of the present invention are as follows:

[0031] Step 1. According to the space mission scenario, build a satellite mission demand model, and digitally represent the perceptual experience knowledge:

[0032] In the traditional satellite mission requirement attribute decision-making process, relying on aerospace experts to infer and make decisions is an abstract process, and it is usually difficult to fully extract and accurately express the rules, methods and thinking modes in the human thinking process. By constructing a qualitative model of satellite mission requirement attributes, a reasonable way is proposed to represent the expert's perceptual experience and knowledge in the decision-making process of satellite mission requirement attribute configuration. The qualitative model is digitally described to realize the digital modeling of typical ae...

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Abstract

The invention relates to a satellite task demand configuration method and system, and the method comprises the following steps: 1, constructing a satellite task demand model according to a space task scene, and carrying out the digital representation of perceptual experience knowledge; 2, performing implicit rule extraction on the spaceflight task sample data, and expanding the spaceflight task data; and step 3, according to a satellite task attribute decision-making method of distance measurement retrieval, obtaining a satellite task demand attribute automatic configuration result. According to the invention, through digital model construction, small sample task data-based implicit rule extraction, sample expansion, satellite task demand intelligent decision algorithm design and the like, satellite task demand intelligent decision is realized; according to the method, the defects that the existing satellite task attribute decision-making process is high in manpower dependence degree, low in processing efficiency, weak in intelligent degree and the like are overcome, and the space task decision-making efficiency and the information support and guarantee capability are improved.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to a method and system for configuring satellite mission requirements based on imitation learning of small sample aerospace mission data. Background technique [0002] At present, there are few studies on the configuration decision of satellite mission requirements attributes. In the research of satellite mission planning and scheduling and other related fields, the satellite mission requirements are usually determined or assumed to be known, that is, the early stage of mission planning based on aerospace information is ignored. The process by which task requirement attribute configuration decisions are made. In the current actual satellite control and mission planning process, the generation and proposal of missions often rely on the experience and knowledge of aerospace experts, and the reasoning and judgment based on information such as targets and environments, so...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06Q10/06G06F16/22G06N3/04G06N3/08
CPCG06Q10/06315G06F16/22G06N3/04G06N3/08
Inventor 王港李玉庆冯小恩高峰雷明佳李娜江飞龙路志勇陈金勇郑怀亮王日新徐敏强
Owner NO 54 INST OF CHINA ELECTRONICS SCI & TECH GRP
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