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A visual detection and evaluation method for micro-impact damage of in-orbit spacecraft

A spacecraft and micro technology, applied in the field of visual detection and evaluation of small impact damage of on-orbit spacecraft, can solve problems such as sensitivity to changes in function values, achieve uniform distribution of optimal solutions, achieve rapidity and effectiveness, and improve clustering accuracy degree of effect

Active Publication Date: 2022-04-19
中国空气动力研究与发展中心超高速空气动力研究所
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

In the original patent, the index representing the degree of change in the dynamic multi-objective environment adopts a simple arithmetic mean value, which makes it too sensitive to extreme function value changes

Method used

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  • A visual detection and evaluation method for micro-impact damage of in-orbit spacecraft
  • A visual detection and evaluation method for micro-impact damage of in-orbit spacecraft
  • A visual detection and evaluation method for micro-impact damage of in-orbit spacecraft

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Experimental program
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Effect test

Embodiment

[0287] In this embodiment, there are two kinds of defects on the test piece, that is, defect 1 filled with material with poor thermal conductivity and defect 2 with perforated back.

[0288] The flow chart of transient thermal response search for infrared thermal image data with large size blocks and variable step size is as follows: figure 2 shown.

[0289] The flow chart of fully adaptive SC-SD spectral clustering algorithm is as follows: image 3 shown.

[0290] In this example, the fuzzy C-means clustering is used to classify the selected transient thermal response results as shown in Figure 4 shown.

[0291] The approximate frontier solution set of defect 1 temperature point, defect 2 temperature point and the temperature point of the material itself obtained by collecting the boundary crossing method based on the penalty item is 1 AP, 2 AP and 3 AP. At the same time, the representative transient thermal response of defect 1 temperature point, defect 2 temperatur...

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Abstract

The invention discloses a visual detection and evaluation method for small impact damage of an in-orbit spacecraft, which comprises the following steps: expressing the thermal image sequence of the spacecraft impact damage specimen acquired by an infrared thermal imager with a three-dimensional matrix; selecting from the three-dimensional matrix The pixel point corresponding to the transient thermal response with the smallest rate of rise; determine the size of the block based on the transient thermal response with the minimum rate of rise; perform block and determine the search step size in the block; select the transient thermal response by block and step size; The selected transient thermal responses are classified; based on the SC-SD spectral clustering algorithm, dynamic prediction is realized and multi-objective optimization is performed to select representatives of each type of transient thermal response; the actual defect category number is discriminated based on the Spearman correlation coefficient, and according to The actual defect category number matrix is ​​changed to obtain a two-dimensional image; the regional convolutional neural network R-CNN is used to extract the features of the two-dimensional image, and the defect feature image of the spacecraft impact damage test piece is obtained, so as to realize the visual detection and evaluation of tiny impact damage .

Description

technical field [0001] The invention belongs to the technical field of spacecraft space debris impact damage detection and evaluation, and more specifically, the invention relates to a visual detection and evaluation method for on-orbit spacecraft micro-impact damage. Background technique [0002] With the continuous development of human space activities, the increasing amount of space debris poses a great threat to human space activities and the safety of on-orbit spacecraft. The problem of space debris has become a gradually developing and serious problem in human space development and practice. Reality. In particular, the huge amount of tiny space debris below the centimeter level that exists in the earth's orbit has become a potential killer that threatens orbiting spacecraft and astronauts due to the inability to effectively monitor, warn, and actively avoid. Space accidents are common. When various spacecraft are impacted by space debris, how to realize the acquisiti...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06V10/762G06V10/764G06K9/62G06N3/04G06V10/46G01N25/72
CPCG01N25/72G06V10/462G06N3/045G06F18/23213G06F18/23G06F18/24
Inventor 黄雪刚谭旭彤殷春石安华罗庆赵君尧柳森
Owner 中国空气动力研究与发展中心超高速空气动力研究所
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