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Large-view-field high-precision structural deformation measurement system in simulated space environment

A technology for simulating space and structural deformation, used in the aerospace field

Active Publication Date: 2021-01-29
BEIJING SATELLITE MFG FACTORY
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Problems solved by technology

[0004] The technical problem of the present invention is to overcome the deficiencies of the prior art and provide a large-field-of-view high-precision structural deformation measurement system in a simulated space environment to solve the problem of large-field-of-view high-precision structural deformation field measurement in a simulated environment

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  • Large-view-field high-precision structural deformation measurement system in simulated space environment

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Embodiment Construction

[0042] In order to make the object, technical solution and advantages of the present invention clearer, the embodiments disclosed in the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0043] Aiming at the problems existing in traditional measurement methods in the application of high-stability structural deformation measurement of spacecraft, the present invention proposes a large-field-of-view high-precision sensor based on the combination of image stitching, large-field scanning, baseline protection, and digital image technology. The structural deformation measurement system solves the problem of large field of view and high-precision structural deformation field measurement in a simulated environment. The invention is suitable for measuring the high-precision deformation field of a large-scale structure in a simulated space environment, and is also suitable for measuring the deformation field of a structure in oth...

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Abstract

The invention discloses a large-field-of-view high-precision structural deformation measurement system in a simulated space environment, and the system comprises a space environment simulation tank body, a mounting bottom plate, a measurement base, a measurement movement mechanism, a measurement movement chute structure, a movement mechanism control circuit, a movement mechanism control software and hardware system, a local environment control and visual measurement circuit, a local environment control and visual measurement software and hardware system and an image acquisition unit, two endsof the measurement base are respectively connected with the space environment simulation tank body and the measurement movement chute structure; the measurement movement mechanism is connected with the measurement movement chute structure; the image acquisition unit and the mounting bottom plate are sequentially arranged below the measurement movement mechanism; the movement mechanism control software and hardware system is connected with the measurement movement mechanism through the movement mechanism control circuit; and the local environment control and visual measurement software and hardware system is connected with the image acquisition unit through the local environment control and visual measurement circuit. According to the invention, the problem of large-view-field high-precision structural deformation field measurement in a simulation environment is solved.

Description

technical field [0001] The invention belongs to the field of aerospace technology, and in particular relates to a large field of view and high-precision structural deformation measurement system in a simulated space environment. Background technique [0002] In order to ensure the stability and reliability of high-precision measurement satellites and space-borne equipment indicators, the load installation datum structure must have high stability characteristics, that is, the structure only produces small deformation or "near-zero deformation" characteristics in the space environment. High-stable structures represented by high-precision solid-surface antennas and precision load supports have a major impact on the accuracy of spacecraft, directly determine the performance of the entire device, and even relate to the success or failure of the mission. In the simulated space environment, high-precision real-time acquisition of its stable performance parameters is the core link a...

Claims

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Application Information

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IPC IPC(8): G01B11/16G01B11/00
CPCG01B11/167G01B11/002
Inventor 唐小军回天力于文涛杨凤龙孙子杰田欣李大松郑立豪
Owner BEIJING SATELLITE MFG FACTORY
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