首页|嫦娥五号双目标联合定轨技术研究

嫦娥五号双目标联合定轨技术研究

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为提升轨道器与上升器在月球交会对接过程中的相对轨道精度,以嫦娥五号双目标联合测量为基础,建立了同波束测量(same beam interferometry,SBI)和星间测量的模型,设计了轨道器与上升器联合的统计定轨算法.利用基准轨道分析了 SBI时延、时延率和微波雷达/激光雷达的测距、测速数据精度,结果表明,嫦娥五号SBI与甚长基线干涉测量精度相当,微波雷达/激光雷达的测距精度为米级.在定轨中建立两目标相对运动关系,能够明显提升相对轨道精度.
Dual-Target Joint Orbit Determination Technology of Chang'E-5
Objectives:The accuracy of relative track between orbiter and ascender can ensure success and safety during the meeting and docking process of Lunar.Methods:Based on dual-target joint measurement of Chang'E-5,we established the same beam interferomery(SBI)measurement and inter-satellite measure-ment model,and designed a statistical orbit determination algorithm combined with orbiter and ascender.Results:We used the reference orbit to analyze delay and delay rate of SBI,and the range and range accuracy of microwave radar/laser radar.The accuracy of SBI is equivalent to that of very long baseline interferometry,and the range accuracy of microwave radar/laser radar is at meter level.Conclusions:By establishing the relative motion relationship between the two targets,the relative orbit accuracy can be sig-nificantly improved in orbit determination.

lunar explorationorbit determinationobservation modelsame beam interferometrymicro-wave radarlaser radar

张宇、段建锋、孔静、曹建峰、韩意、李翠兰、宋辰、陈明

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北京航天飞行控制中心,北京,100094

月球探测 定轨 观测建模 同波束测量 微波雷达 激光雷达

国家自然科学基金国家自然科学基金国家自然科学基金

118720344180401911973015

2024

武汉大学学报(信息科学版)
武汉大学

武汉大学学报(信息科学版)

CSTPCD北大核心
影响因子:1.072
ISSN:1671-8860
年,卷(期):2024.49(6)
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