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Moon scientific research station parameterization design and multi-objective optimization method for in-situ construction

A parametric design and multi-objective optimization technology, applied in multi-objective optimization, special data processing applications, geometric CAD, etc., can solve the problems of complex parameter modification, complex structural design model design, etc., to achieve shortened design cycle, reliable design and The effect of optimizing method and reducing development cost

Pending Publication Date: 2022-02-08
HUAZHONG UNIV OF SCI & TECH
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Problems solved by technology

[0003] Aiming at the above defects or improvement needs of the prior art, the present invention provides a parametric design and multi-objective optimization method for the in-situ construction of the lunar scientific research station, thereby solving the problem that the structure design model of the existing lunar scientific research station is complicated and Complex problem of parameter modification for optimization of structures for multiple specific objectives

Method used

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  • Moon scientific research station parameterization design and multi-objective optimization method for in-situ construction
  • Moon scientific research station parameterization design and multi-objective optimization method for in-situ construction
  • Moon scientific research station parameterization design and multi-objective optimization method for in-situ construction

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[0041] In order to make the objects, technical solutions and advantages of the present invention, the present invention will be described in detail below with reference to the accompanying drawings and examples. It is to be understood that the specific embodiments described herein are intended to explain the present invention and is not intended to limit the invention. Moreover, various embodiments of the invention described below involved the technical features as long as no conflict with one another can be configured in combination with each other.

[0042] Example embodiments provide lunar research station parameters and multi-objective optimization design method for in-situ for the building of the present invention, as figure 1 As shown, including:

[0043] S1, determining a plurality of variable parameters based on the shape of the moon structures Research Station desired construction.

[0044] Preferably, as Figure 2-3 , The shape of the Research Station for double-moon shap...

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Abstract

The invention discloses a moon scientific research station parameterization design and multi-objective optimization method for in-situ construction. The method includes: designing corresponding structure parameter variables according to the shape of the required moon scientific research station, achieving structure parameter optimization under multiple objectives, obtaining an optimal solution by solving a multi-objective function,namely the optimal structure parameters of the moon scientific research station, wherein the obtained optimal structure parameters can be directly applied to the in-situ resource 3D printing of the moon, so that the in-situ 3D printing of the moon scientific research station is realized. An efficient and reliable design and optimization method is provided for the in-situ construction-oriented structural design of the moon scientific research station, the design period of the moon scientific research station can be shortened, and the development cost can be reduced.

Description

Technical field [0001] The present invention belongs to the field of optimization of parametric design and architectural structures, and more particularly, to a construction for the in-situ lunar research station parameters and design method of multi-objective optimization. Background technique [0002] With the completion of my country's space technology development and lunar exploration, the use of the moon on the moon in situ resources to build lunar research station will be an important goal of the next phase of lunar exploration project. For Moon microgravity, large temperature changes and micro-meteorite impacts associated with harsh environment, the structure of the lunar research station design has become an important task. Generating a velocity model of traditional design methods lunar research station configuration slow, very complex modifications, low efficiency and difficult to optimize the structure for a plurality of specific targets. Inventive content [0003] To ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/13G06F111/06
CPCG06F30/13G06F2111/06
Inventor 周诚丁烈云陈权要韩文彬
Owner HUAZHONG UNIV OF SCI & TECH
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