大载荷通信卫星多学科设计与元模型辅助优化

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2024-12-31 DOI:10.1016/j.actaastro.2024.12.042
Renhe Shi, Xinhui Tai, Teng Long, Nianhui Ye, Fuxiang Dong
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引用次数: 0

摘要

随着高速数据传输和全球通信需求的不断提高,具有大尺寸天线载荷的地球同步轨道通信卫星备受关注。为了解决有效系统设计的挑战,本文提出了一种基于元模型的大型有效载荷通信卫星多学科设计优化框架。在此框架下,在若干实际工程约束条件下,提出了最小化系统总质量的LSP-TS MDO问题。考虑大载荷与卫星平台的相互关联关系,建立了卫星几何构型、动力、姿态控制、结构、地球静止轨道保持、轨道转移和质量学科的分析模型。为了降低计算成本,提出了一种基于Pareto适应度采样(AKM-PFS)的自适应Kriging方法作为与卫星MDO框架相结合的优化器。该方法通过探索目标和约束的Pareto边界,构建LSP-TS系统的Kriging元模型,并对其进行自适应优化,从而有效地搜索到可行的优化卫星系统设计。优化后的系统总质量比满足所有约束条件的初始解降低了318.53 kg(8.87%)。进一步讨论了所提AKM-PFS的优化解,说明了所提方法的实用性和有效性。
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Multidisciplinary design and metamodel assisted optimization for a telecommunication satellite with large-size payload
With the increasing demands for high-speed data transmission and global communication, GEO telecommunication satellites with large-size antenna payload have attracted much attention nowadays. To address the challenge of effective system design, this paper proposes a metamodel assisted multidisciplinary design optimization (MDO) framework for a Large-size Payload Telecommunication Satellite (LSP-TS). In the framework, the LSP-TS MDO problem is formulated to minimize the total system mass subject to several practical engineering constraints. Considering the interconnected relationship between the large-size payload and the satellite platform, the analysis models of satellite geometry configuration, power, attitude control, structure, GEO station-keeping, orbital transfer, and mass disciplines are established. To reduce the computational cost, an adaptive Kriging method using Pareto fitness-based sampling (AKM-PFS) is proposed as the optimizer integrated with the satellite MDO framework. In this approach, the Kriging metamodels of LSP-TS system are constructed and adaptively refined for optimization via exploring the Pareto frontier of objective and constraints, which leads the search to the feasible optimized satellite system design efficiently. After optimization, the total system mass is reduced by 318.53 kg (8.87 %) compared with the initial solution where all constraints being satisfied. Moreover, the optimization solution of the proposed AKM-PFS is further discussed to illustrate the practicality and effectiveness of the proposed method.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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