北京航空航天大学学报 ›› 2020, Vol. 46 ›› Issue (7): 1405-1411.doi: 10.13700/j.bh.1001-5965.2019.0437

• 论文 • 上一篇    下一篇

基于可视化模型的可重构航天器概念设计方法

郭达维1, 刘莉1, 陈余军2, 李文光1, 程松1   

  1. 1. 北京理工大学 宇航学院, 北京 100081;
    2. 中国空间技术研究院 通信卫星事业部, 北京 100094
  • 收稿日期:2019-08-12 发布日期:2020-07-18
  • 通讯作者: 刘莉 E-mail:liuli@bit.edu.cn
  • 作者简介:郭达维 男,硕士研究生。主要研究方向:飞行器总体设计、飞行器结构分析与设计。
    刘莉 女,博士,教授,博士生导师。主要研究方向:飞行器总体设计、飞行器结构设计与强度分析、飞行器制导与控制技术。

Conceptual design method of reconfigurable spacecraft based on visualization model

GUO Dawei1, LIU Li1, CHEN Yujun2, LI Wenguang1, CHENG Song1   

  1. 1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China;
    2. Institute of Telecommunication Satellite, China Academy of Space Technology, Beijing 100094, China
  • Received:2019-08-12 Published:2020-07-18

摘要: 针对可重构航天器需要考虑几何和性能双重约束的特点,为了充分发挥概念设计阶段具有较大创新空间的优势,提出了一种基于可视化模型的可重构航天器概念设计方法,给出了具有良好开放性和可扩展性的平台体系框架,搭建了具有高真实度交互界面和快速性能评估功能的可重构航天器概念设计平台,可实现不同可重构航天器构型的拼装。算例表明,所提出的概念设计方法可以满足可重构航天器的概念设计需求,搭建的平台能为可重构航天器概念设计方案论证提供条件保障。

关键词: 可重构航天器, 卫星设计, 概念设计, 性能评估, 可视化

Abstract: In order to give full play to the advantages of innovation in the conceptual design stage, and to satisfy the dual constraints of geometry and performance for the reconfigurable spacecraft, a conceptual design method of reconfigurable spacecraft based on visualization model is proposed. The architecture with openness and extensibility of the conceptual design platform was given, and the platform was built with high-reality interactive interface and rapid performance evaluation function, which can realize the assembly of different configurations of reconfigurable spacecraft. The computational example shows that the proposed conceptual design method can meet the conceptual design requirements of reconfigurable spacecraft, and the developed platform can provide conditions for the conceptual design scheme argumentation of reconfigurable spacecraft.

Key words: reconfigurable spacecraft, satellite design, conceptual design, performance evaluation, visualization

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