航天器工程2024，Vol.33Issue(2)：16-20,5.DOI:10.3969/j.issn.1673-8748.2024.02.003
低轨星座卫星快速开发与验证方案设计
Rapid Development and Verification Scheme Design of LEO Constellation Satellite
刘敏 1范为 1裴胜伟 1李峰1
作者信息
- 1. 中国空间技术研究院通信与导航卫星总体部,北京 100094
- 折叠
摘要
Abstract
Aiming at meeting the rapid development and verification needs of LEO(low earth or-bit)constellation satellite,the parallel development and verification scheme of engineering satel-lite model and a VPI(verification platform interface)and experimental satellite is proposed.Through the development of engineering satellite model,the design of structure subsystem,as-sembly and the main design of power supply and propulsion subsystem are verified to support the optimization of experimental satellite design and the commissioning of main structure.VPI vali-dates of equipment electrical interface and software.Through experimental satellite develop-ment,the functional performance of LEO constellation satellite is comprehensive verified,and the baseline of satellites is established.The verification scheme is implemented in satellites,and is proved that it can effectively improve the verification efficiency of LEO constellation satellite.关键词
低轨星座卫星/工程星/快速开发/设计验证Key words
LEO constellation satellite/engineering satellite model/rapid development/design veri-fication分类
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刘敏,范为,裴胜伟,李峰..低轨星座卫星快速开发与验证方案设计[J].航天器工程,2024,33(2):16-20,5.
