李朵朵, 周旭华, 李凯, 徐可馨, 陶恩哲. HY2B星载GPS精密定轨研究[J]. 武汉大学学报 ( 信息科学版), 2023, 48(12): 2060-2068. DOI: 10.13203/j.whugis20210303
引用本文: 李朵朵, 周旭华, 李凯, 徐可馨, 陶恩哲. HY2B星载GPS精密定轨研究[J]. 武汉大学学报 ( 信息科学版), 2023, 48(12): 2060-2068. DOI: 10.13203/j.whugis20210303
LI Duoduo, ZHOU Xuhua, LI Kai, XU Kexin, TAO Enzhe. Precise Orbit Determination for HY2B Using On-Board GPS Data[J]. Geomatics and Information Science of Wuhan University, 2023, 48(12): 2060-2068. DOI: 10.13203/j.whugis20210303
Citation: LI Duoduo, ZHOU Xuhua, LI Kai, XU Kexin, TAO Enzhe. Precise Orbit Determination for HY2B Using On-Board GPS Data[J]. Geomatics and Information Science of Wuhan University, 2023, 48(12): 2060-2068. DOI: 10.13203/j.whugis20210303

HY2B星载GPS精密定轨研究

Precise Orbit Determination for HY2B Using On-Board GPS Data

  • 摘要: 海洋二号B星(Haiyang-2 B,HY2B)是中国海洋动力环境监测的首颗组网卫星,主要用于探测海面高度、海面风场、重力场等多种海洋动力环境参数,高精度卫星轨道是完成上述任务的前提与关键。选取HY2B卫星2021年1月的星载GPS观测数据,从数据完整性与多路径效应两个方面分析了观测质量,采用简化动力学定轨方法进行了精密定轨研究。结果显示,相比海洋二号A星(Haiyang-2 A,HY2A),搭载同一型号接收机的HY2B卫星伪距多路径误差有所下降;基于国产星载双频GPS接收机可以实现HY2B卫星径向2 cm、三维优于3 cm的定轨精度;同时,验证了相位中心变化(phase center variation,PCV)模型对精密定轨的改进作用。目前的星载GPS数据与定轨方法可以满足高精度海洋测高任务的需求。

     

    Abstract:
    Objectives Haiyang-2 B(HY2B), launched on 24 October 2018, is the first satellite of Chinese marine dynamic environment monitoring mission. It is mainly used to detect various marine dynamic environmental parameters such as sea surface height, sea surface wind field, and gravity field.
    Methods Precise orbit tracking and determination is very key for the mission. The reduced-dynamic precise orbit determination for HY2B was carried out utilizing the spaceborne GPS observation in January 2021 and the orbit accuracy was evaluated by means of four methods.
    Results The results show that: (1) The average value of the carrier phase fitting residual is about 7.2 mm, and the three-dimensional position difference between adjacent arcs of 28 h orbit determination overlapping for 4 h is less than 1.5 cm. (2) Compared with the precision orbit ephemerides (POE) issued by Centre National d'Etudes Spatiales (CNES), the root mean square (RMS) average values of the difference in direction radial, along-track, cross-track and three-dimensional(3D) position are 1.5 cm, 2.0 cm, 1.4 cm and 2.9 cm, respectively. (3)The satellite laser ranging validation statistics RMS is about 2 cm. (4) By applying phase center variation model constructed by residual method, the 3D RMS difference with CNES POE product is reduced from 3 cm to 2.5 cm.
    Conclusions In conclusion, high-precision HY2B satellite orbit products can be obtained basing on space-borne GPS observation of the HY2B satellite.

     

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