“北京三号”C卫星构型布局设计与优化  

Design and optimization of configuration layout for BJ-3C Satellite

作　　者：阮伟靖 张一鹏 吴止境 马灵犀[1] 唐斌 孟晓亮[1] RUAN Weijing;ZHANG Yipeng;WU Zhijing;MA Lingxi;TANG Bin;MENG Xiaoliang(DFH Satellite Co.,Ltd.,Beijing 100094,China)

机构地区：[1]航天东方红卫星有限公司,北京100094

出　　处：《先进小卫星技术(中英文)》2025年第2期59-64,共6页Advanced Small Satellite Technology

摘　　要：针对“北京三号”C卫星快速机动、轻量化和批量发射的任务特点,对卫星构型布局进行了设计与优化,包括卫星低惯量轻量化构型设计、主传力路径优化设计、载荷与平台解耦设计、整星微振动抑制及卫星构型与运载发射构型的匹配性设计.“北京三号”C卫星在轨飞行验证结果表明:卫星构型布局设计合理可靠,满足任务需求,可为后续同类卫星的构型布局设计提供参考.The configuration layout of the satellites was designed and optimized with the mission characteristics of the BJ-3C Satellite,such as rapid maneuverability,lightweight and batch-launch.The design of a low-inertia lightweight configuration,main force-transmission path optimization,payload and platform decoupling,satellite-level micro-vibration suppression and compatibility of the satellites with the launch vehicle were included in this configuration layout.The in-orbit flight verification of the BJ-3C Satellite shows that the satellite configuration layout design is reasonable and reliable while meeting the mission requirements,and can provide references for the subsequent configuration layout design of similar satellites.

关 键 词：“北京三号”C卫星 构型布局设计 光学卫星星座 轻量化敏捷卫星 

分 类 号：V423.4[航空宇航科学与技术—飞行器设计]