翟振和, 孙中苗, 肖云, 李芳. 自主海洋测高卫星串飞模式的设计与重力场反演精度分析[J]. 武汉大学学报 ( 信息科学版), 2018, 43(7): 1030-1035, 1128. DOI: 10.13203/j.whugis20160234
引用本文: 翟振和, 孙中苗, 肖云, 李芳. 自主海洋测高卫星串飞模式的设计与重力场反演精度分析[J]. 武汉大学学报 ( 信息科学版), 2018, 43(7): 1030-1035, 1128. DOI: 10.13203/j.whugis20160234
ZHAI Zhenhe, SUN Zhongmiao, XIAO Yun, LI Fang. Two-Satellites Tandem Mode Design and Accuracy Analysis of Gravity Field Inversion for Independent Marine Altimetry Satellite[J]. Geomatics and Information Science of Wuhan University, 2018, 43(7): 1030-1035, 1128. DOI: 10.13203/j.whugis20160234
Citation: ZHAI Zhenhe, SUN Zhongmiao, XIAO Yun, LI Fang. Two-Satellites Tandem Mode Design and Accuracy Analysis of Gravity Field Inversion for Independent Marine Altimetry Satellite[J]. Geomatics and Information Science of Wuhan University, 2018, 43(7): 1030-1035, 1128. DOI: 10.13203/j.whugis20160234

自主海洋测高卫星串飞模式的设计与重力场反演精度分析

Two-Satellites Tandem Mode Design and Accuracy Analysis of Gravity Field Inversion for Independent Marine Altimetry Satellite

  • 摘要: 根据自主海洋测高卫星发展需求,设计了双星串飞运行模式,该运行模式下2.3 a时间可满足全球海洋区域1'×1'分辨率的地面轨迹覆盖要求。首先,将测高卫星重力场反演分为不考虑轨道运行特点(思路1)和考虑串飞轨道运行特点(思路2)两种思路,利用逆Vening-Meinesz方法开展了正态分布下随机误差传播的仿真计算,获得了两种思路下对应的误差指标。以该误差指标为基础,分别计算了双星串飞模式下两种重力场反演思路对应的精度指标。其中,反演思路2充分利用了串飞模式双星东西方向地面观测值可以进行相对定轨的特点,并考虑到近距离条件下传播误差、地球物理改正误差的系统误差特性,因此反演思路2的垂线偏差精度较反演思路1有了一定的提高,其重力场反演也具有一定的优势。理论计算结果表明,利用思路1的反演方法,2.3 a时间可获得1'×1'重力异常精度为6~10 mGal,4.6 a时间可达到4.2~7.1 mGal;利用思路2的反演方法,2.3 a时间可获得1'×1'重力异常精度为3.9 mGal,4.6 a时间可达到2.8 mGal。

     

    Abstract: In order to meet the future development requirements of independent altimetry satellite, a two-satellites tandem mode is designed which can cover the whole ocean area with 1'×1' resolution after 2.3 years of flying. Firstly, two gravity field inversion methods for independent marine altimetry satellite are proposed, one of which takes the tandem orbital characteristics into account while the other does not. Secondly, the simulation calculation of random error propagation under normal distribution is carried out by using the inverse Vening-Meinesz method, and the corresponding indices of error under the two approaches are obtained.Based on the above error indexes, the corresponding precision indexes of the two kinds of gravity field inversion methods in the tandem flight mode are calculated respectively.Among, the second inversion method makes full use of the characteristics of the relative orbit determination by using the east-west observations in the tandem mode, and takes account of the systematic error characteristics of the propagation error and geophysical correction error under the close-range conditions. Therefore, the vertical deflection accuracy of the second inversion method is higher than that of the first inversion method, and its gravity field inversion also has certain advantages accordingly.The theoretical calculation results show that using the first inversion method, we can get a gravity anomaly accuracy of 6-10 mGal in 2.3 yearsand 4.2-7.1 mGal in 4.6 years; while using the second inversion method, a gravity anomaly accuracy of 3.9 mGal in 2.3 years and 2.8 mGal in 4.6 years can be obtained, respectively.

     

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