| 注册
首页|期刊导航|航空学报|基于融合代理策略的超声速降落伞气动优化设计

基于融合代理策略的超声速降落伞气动优化设计

姜璐璐 潘鑫 蒋伟 冯瑞 陈刚

航空学报2025,Vol.46Issue(1):71-85,15.
航空学报2025,Vol.46Issue(1):71-85,15.DOI:10.7527/S1000-6893.2024.30471

基于融合代理策略的超声速降落伞气动优化设计

Optimization shape design of capsule-supersonic parachute system based on fusion surrogate strategy

姜璐璐 1潘鑫 1蒋伟 2冯瑞 2陈刚1

作者信息

  • 1. 西安交通大学 航天航空学院,西安 710049||机械结构强度与振动国家重点实验室,西安 710049||陕西省先进飞行器服役环境与控制重点实验室,西安 710049
  • 2. 北京空间机电研究所,北京 100094
  • 折叠

摘要

Abstract

Supersonic parachutes,as crucial aerodynamic deceleration systems providing drag and stability,directly impact the success of lander missions.The structural parameters of parachutes that meet different aerodynamic per-formance requirements are often contradictory.To address the issues of structural parameter conflicts in the shape de-sign of Mars parachutes,as well as the errors of lengthy design cycles and high calculation,this study proposes a fu-sion surrogate optimization strategy for the two-body model of the canopy-capsule system.The fusion surrogate model integrates the advantages of interpolation-based and regression-based surrogate models,and achieves higher predic-tion accuracy of aerodynamic coefficients under the same sample conditions.By employing the fusion surrogate model to replace the time-consuming Computational Fluid Dynamics(CFD)calculation process,the design cycle can be shortened,and design efficiency can be improved.The two-body model of the capsule-DGB parachute is optimized using a multi-objective genetic algorithm.The results show that the fusion surrogate optimization strategy can balance the drag and stability performance of the canopy,and enhance the overall deceleration capability of the disk-gap-band parachute under structural parameters and aerodynamic constraints,demonstrating good practicality and feasibility.The research findings can provide theoretical reference and technical reserves for the design and development of a new generation of supersonic parachutes for future Mars exploration missions.

关键词

融合策略/火星降落伞/优化设计/代理模型/超声速

Key words

fusion strategy/Mars parachute/optimization design/surrogate model/supersonic

分类

航空航天

引用本文复制引用

姜璐璐,潘鑫,蒋伟,冯瑞,陈刚..基于融合代理策略的超声速降落伞气动优化设计[J].航空学报,2025,46(1):71-85,15.

基金项目

国家自然科学基金(92371201,52192633,9215230) (92371201,52192633,9215230)

陕西省自然科学基金(2022JC-03) National Natural Science Foundation of China(92371201,52192633,9215230) (2022JC-03)

Natural Science Foundation of Shaanxi Province(2022JC-03) (2022JC-03)

航空学报

OA北大核心

1000-6893

访问量0
|
下载量0
段落导航相关论文