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System design and validation of Queqiao-2 lunar relay communication satellite
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作者 ZHANG Lihua XIONG Liang +11 位作者 SUN Ji CHEN Luojing XIAO Chuan ZHOU Wenyan WANG Yong LIU Wangwang GUAN Yifeng CHEN Tao YU Xiaochuan XU Jin CHEN Guohui CAO Xiaoping 《中国空间科学技术(中英文)》 CSCD 北大核心 2024年第5期23-39,共17页
In order to provide relay communication supports for future Chinese lunar exploration program,Queqiao-2 relay communication satellite was developed.Queqiao-2 can perform scientific observations with three kinds of sci... In order to provide relay communication supports for future Chinese lunar exploration program,Queqiao-2 relay communication satellite was developed.Queqiao-2 can perform scientific observations with three kinds of scientific instruments on board.The system design of Queqiao-2,including mission orbit and transfer orbit design,configuration and layout design,housekeeping and information flow design,power supply and distribution design,GNC and propulsion system design,communication links design,etc.,was accomplished through comprehensive tradeoff and evaluation on technical maturity,availability,schedule,cost,and so on.With a view to reducing development risk,both the platform and relay communication payloads were developed based on significant heritage from previous Queqiao relay satellite and other relevant spacecraft.Queqiao-2 features flexible system architecture to support multiple frequencies,modulations,data rates and software reconfigurations to meet new user requirements.Subsequent to a successful launch on March 20,2024,by means of 5 orbit maneuvers,Queqiao-2 was inserted into a highly elliptical frozen mission orbit around the moon with a 24h period on schedule.Following on-orbit tests and calibrations,Queqiao-2 has possessed the capacity to provide reliable relay communication services to multiple lunar exploration missions,as well as the capacity to perform scientific observations.Under the support of Queqiao-2,Chang′e-6 achieved its ambitious mission goal to collect and return samples from the moon′s mysterious far side.In the meanwhile,Queqiao-2 has also paved the way for the following Chinese lunar exploration missions including Chang′e-7 and Chang′e-8.The design life time of Queqiao-2 is more than 8 years.Benefit from flexibility and extensibility of relay communication system design,it is convenient to provide relay communication services for future lunar exploration missions of both China and other countries.In addition,innovative scientific observations would be performed during the period that no relay communication task is arranged.The system design of Queqiao-2 reflects the development philosophy of technical innovations and inheritance integration.Based on highly flexible and extensible system architecture,multiple and concurrent relay communication mission requirements can be met.It can provide strong supports for future lunar exploration missions.Successful launching,orbit entering and on-orbit tests of Queqiao-2 verified the correct design principle and versatility.By means of Queqiao-2,more innovative scientific outcomes are anticipated and lunar exploration activities can be facilitated. 展开更多
关键词 lunar explorations relay communication queqiao system design TEST VALIDATION
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One Year On-orbit Operation of Queqiao Lunar Relay Communications Satellite 被引量:2
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作者 ZHANG Lihua XIONG Liang +1 位作者 SUN Ji CHEN Luojing 《Aerospace China》 2019年第3期5-13,共9页
Queqiao relay communications satellite was developed to provide relay communications services for the lander and the rover on the far side of the moon. From entering into its halo mission orbit around the Earth-moon l... Queqiao relay communications satellite was developed to provide relay communications services for the lander and the rover on the far side of the moon. From entering into its halo mission orbit around the Earth-moon libration point 2 on June 14, 2018, it has operated on orbit more than fifteen months. It worked very well and provided reliable, continuous relay communications services for the lander and the rover to accomplish the goals of Chang’e 4 lunar far side soft landing and patrol exploration mission. The on-orbit operation status of Queqiao relay communications satellite is summarized in this paper. 展开更多
关键词 Chang'e 4 mission queqiao RELAY COMMUNICATIONS FAR SIDE of the MOON
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深空测控网干涉测量系统在“鹊桥”任务中的应用分析 被引量:5
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作者 王美 陈略 +4 位作者 韩松涛 路伟涛 段建锋 任天鹏 李黎 《深空探测学报》 2018年第6期539-543,共5页
在"嫦娥4号"任务的第一阶段—"鹊桥"阶段,北京航天飞行控制中心利用佳木斯及喀什深空站对"鹊桥"进行了干涉测量观测,获取了实时与事后的高精度测角观测量,有效支持了任务的实施。两深空站需同时完成测控... 在"嫦娥4号"任务的第一阶段—"鹊桥"阶段,北京航天飞行控制中心利用佳木斯及喀什深空站对"鹊桥"进行了干涉测量观测,获取了实时与事后的高精度测角观测量,有效支持了任务的实施。两深空站需同时完成测控任务,无法交替射电源观测来进行系统差标校,基于此系统采用了长时间隔、在航天器观测前及双站结束后观测射电源的标校方法,在地月转移段、月球至L2转移段、Halo轨道形成段开展了多次干涉测量观测,所获得的时延、时延率结果直接应用于事后联合轨道确定,结果表明:深空网的时延观测精度约为3 ns。 展开更多
关键词 干涉测量 鹊桥 定轨评估
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服务轨道维持“鹊桥”计算精度的评估
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作者 孔静 谢剑锋 +4 位作者 胡国林 刘俊琦 马传令 吴舒然 李柯 《深空探测学报(中英文)》 CSCD 北大核心 2023年第6期652-658,共7页
位于地月L2点Halo轨道的“嫦娥四号”中继星,每3~4天需要通过动量轮卸载和轨道维持两种方式进行构型保持。针对“嫦娥四号”中继星机动频繁、控制精度高的特点,根据平动点轨道特性,在旋转坐标系分析了定轨误差分量对轨道控制参数计算的... 位于地月L2点Halo轨道的“嫦娥四号”中继星,每3~4天需要通过动量轮卸载和轨道维持两种方式进行构型保持。针对“嫦娥四号”中继星机动频繁、控制精度高的特点,根据平动点轨道特性,在旋转坐标系分析了定轨误差分量对轨道控制参数计算的影响,得出影响轨道维持效果的定轨误差主要为旋转坐标系X-Y平面的速度误差。在此基础上提出一种服务轨道维持控制定轨精度评估的统计学方法,设计了平动点飞行期间轨道的计算策略,对中继星使命轨道的定轨精度开展评估,结果表明,目前测量条件下可为轨道维持提供的定轨精度为1~3mm/s。 展开更多
关键词 “鹊桥” 轨道维持 旋转坐标系 轨道确定 精度评估
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地月系平动点轨道动力学建模与控制策略研究 被引量:3
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作者 于登云 周文艳 高珊 《航天器工程》 CSCD 北大核心 2019年第2期9-18,共10页
根据嫦娥四号探测器开展月球背面探测的中继通信需求,基于地月系平动点特性,建立考虑三体引力的高精度动力学模型,给出不同飞行阶段的轨道求解方法。在动力学模型和求解方法基础上,结合嫦娥四号"鹊桥"中继卫星的轨道设计,提... 根据嫦娥四号探测器开展月球背面探测的中继通信需求,基于地月系平动点特性,建立考虑三体引力的高精度动力学模型,给出不同飞行阶段的轨道求解方法。在动力学模型和求解方法基础上,结合嫦娥四号"鹊桥"中继卫星的轨道设计,提出了最佳轨道方案和轨道控制策略。"鹊桥"卫星的飞行实践结果表明:动力学建模及轨道设计结果正确,满足中继任务需求,相关模型和方法可为未来平动点任务提供参考。 展开更多
关键词 地月系平动点 HALO轨道 动力学建模 轨道控制策略 “鹊桥”中继卫星
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Chang'e 4's Relay Satellite Bridging Earth and Moon
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作者 YU Guobin 《Aerospace China》 2019年第2期40-45,共6页
The far side of the moon is a unique place for some scientific investigations.Chang'e 4 is a Chinese lunar far side landing exploration mission.Relay communication satellite,named as Queqiao,is an important and in... The far side of the moon is a unique place for some scientific investigations.Chang'e 4 is a Chinese lunar far side landing exploration mission.Relay communication satellite,named as Queqiao,is an important and innovative part of Chang'e 4 mission.It can provide relay communication to the lander and the rover operating on the lunar far side to maintain their contacts with Earth.It was launched by LM-4C launch vehicle at the Xichang Satellite Launch Center on May 21,2018.After five precise orbit controls and a journey of more than 20 days,Queqiao inserted into final halo mission orbit around Earth-moon libration point 2,located about 65,000 km beyond the moon.It is the world's first communication satellite operating in that orbit.Up to now,Queqiao worked very well and provided reliable,continuous communication relay service for the lander and the rover to ensure the mission success of Chang'e 4 exploration mission.Via Queqiao,the lander and the rover were controlled to work by ground stations and obtained a great amount of scientific data.The mission overview,operation orbit selection,relay communication system design and flight profile were introduced in this article. 展开更多
关键词 Chang'e 4 mission queqiao LUNAR far side RELAY communications Earth-moon LIBRATION point 2
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鹊桥中继星-北斗导航卫星的单链路星间自主定轨 被引量:1
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作者 陈思睿 杜兰 《测绘科学技术学报》 北大核心 2020年第4期362-367,共6页
星间链路ISL(Inter-Satellite Link)测距测速是导航星座自主定轨的主要数据来源。当星座仅涉及传统二体问题意义下的卫星时,ISL定轨是秩亏的。若引进地月系平动点轨道飞行器,则有望解决扩展星座的自主定轨。本文探讨了联合嫦娥四号的“... 星间链路ISL(Inter-Satellite Link)测距测速是导航星座自主定轨的主要数据来源。当星座仅涉及传统二体问题意义下的卫星时,ISL定轨是秩亏的。若引进地月系平动点轨道飞行器,则有望解决扩展星座的自主定轨。本文探讨了联合嫦娥四号的“鹊桥”中继卫星与北斗导航星座的自主联合定轨方法。分别构建了“鹊桥”与北斗混合星座中3类轨道卫星的星间测距单链路,数值分析表明,引入“鹊桥”卫星的定轨法矩阵的条件数约减小3个数量级,大大削弱了法矩阵的病态性。EKF自主定轨的滤波收敛后,除GEO的Z分量外,3类北斗卫星的自主定轨结果均可将初轨误差减小50%,但“鹊桥”中继星的轨道改进程度不如北斗卫星。若以“鹊桥”作为空间基准仅解算北斗导航卫星轨道,GEO定轨精度可达m级。仿真结果可为北斗导航星座星间链路的拓展应用提供一种新思路。 展开更多
关键词 鹊桥 HALO轨道 北斗导航星座 自主定轨 星间链路
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牛郎织女恨 《鹊桥仙》中情——宋代《鹊桥仙》七夕相会词的情感内涵及审美效应 被引量:1
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作者 卢小燕 《四川教育学院学报》 2007年第5期43-46,共4页
宋代《鹊桥仙》中的七夕相会词包涵着丰富的情感内涵,众多佳作将情感世界里重逢的喜悦、别离的忧伤、思念的恒久和等待的执著等一系列情感内容艺术性地加以展现,带给人以悲剧性的审美快感,并在超越悲剧的意味上给人以思想的启迪和精神... 宋代《鹊桥仙》中的七夕相会词包涵着丰富的情感内涵,众多佳作将情感世界里重逢的喜悦、别离的忧伤、思念的恒久和等待的执著等一系列情感内容艺术性地加以展现,带给人以悲剧性的审美快感,并在超越悲剧的意味上给人以思想的启迪和精神的振奋。 展开更多
关键词 牛郎织女 《鹊桥仙》 七夕相会 情感内涵 审美效应
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鹊桥二号星务分系统信息传输多路径设计
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作者 刘子杰 闫国瑞 +1 位作者 高若辰 王啟宁 《先进小卫星技术(中英文)》 2024年第4期41-51,共11页
鹊桥二号作为地月通信中继卫星,其意义在于能够在地球和月球之间建立稳定的信息交换通路,使得月球背面探测器与地面站之间能够进行信息交换,获取珍贵的探测数据和样本.提出了鹊桥二号星务分系统多路径信息处理技术,设计了高速遥控通道... 鹊桥二号作为地月通信中继卫星,其意义在于能够在地球和月球之间建立稳定的信息交换通路,使得月球背面探测器与地面站之间能够进行信息交换,获取珍贵的探测数据和样本.提出了鹊桥二号星务分系统多路径信息处理技术,设计了高速遥控通道与低速遥控通道信息流传输方案,高速遥控通道支持大规模软件上注更新,也可作为低速遥控通道的备份,实现了遥控多路径.此外,提出了一般遥测、详细遥测及应急遥测等遥测多路径和多模式设计,增强了卫星的可靠性、灵活性和适应性.该技术实现了对嫦娥六号月背采样返回任务及嫦娥四号中继通信的支持,在为期一个多月的嫦娥六号任务中,执行并转发了超过2000条指令,有效保障了任务顺利完成,并具备对未来嫦娥七号和嫦娥八号任务提供通信保障的能力. 展开更多
关键词 鹊桥二号 星务分系统 在轨维护 高速上注 中继通信
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