测绘学报

• 学术论文 • 上一篇    下一篇

基于MGS测图段部分弧段的精密定轨及火星重力场模型解算

鄢建国1,李斐2,平劲松3   

  1. 1. 武汉大学测绘遥感信息工程国家重点实验室
    2. 武汉大学信息学部测绘遥感信息工程国家重点实验室
    3. 中国科学院上海天文台
  • 收稿日期:2010-01-05 修回日期:2010-04-02 出版日期:2010-10-25 发布日期:2010-10-25
  • 通讯作者: 鄢建国

Precision Orbit Determination of MGS Mapping Phase Arcs and Martian Gravity Field Model Solution

, ,   

  • Received:2010-01-05 Revised:2010-04-02 Online:2010-10-25 Published:2010-10-25

摘要: 火星探测器精密定轨关联到火星探测任务的成功实施并为其科学目标的顺利完成提供保障,火星重力场研究除了为精密定轨服务外,还是进行火星内部结构、火星表面质量迁移及火星形成和演化的重要约束条件。基于火星探测器精密定轨及火星重力场研究的重要意义,本文利用MGS(Mars Global Surveyor)测图任务阶段近两个月的轨道跟踪数据进行了解算分析,对精密定轨结果进行了精度评价。在此基础上,进行了火星重力场模型解算,通过轨道残差、火星自由空气重力异常等方式对解算模型进行了精度评价,结果表明解算模型合理。这一研究为我国即将发射的火星探测计划“萤火一号”轨道跟踪数据用于火星重力场研究打下了基础。

Abstract: POD (Precision orbit determination) of Mars exploration spacecraft is vital to its mission and scientific objects implementation. Besides using for POD, Martian gravity field is an important constraint for researches about Mars internal structure, Mars surface mass transformation and Mars origin and revolutionary. Considering the importance of Mars spacecraft POD and Martian gravity field, POD of MGS (Mars Global Surveyor) is done using nearly two months tracking data during mapping phase, and the accuracy of orbital result is evaluated by orbital overlap analysis. In following Martian gravity field model is solved, and the model accuracy is assessed by methods such as gravity power spectrum, orbital residuals and Mars free-air gravity anomaly, the results show the reasonability of the solution, and dominating Martian gravity field information can be extracted by nearly two months tracking data. The work lays foundation for application of our national Mars exploration mission “YH-1” tracking data in Martian gravity field research..