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基于星载GPS的HY-2卫星高精度精密定轨模拟研究(英文)
引用本文:郭金运,秦建,孔巧丽,李国伟.基于星载GPS的HY-2卫星高精度精密定轨模拟研究(英文)[J].应用地球物理,2012,9(1):95-107.
作者姓名:郭金运  秦建  孔巧丽  李国伟
作者单位:山东科技大学测绘学院;海岛(礁)测绘技术国家测绘地理信息局重点实验室
基金项目:supported partially by the National Natural Science Foundation of China (Nos. 40974004 and 40974016);Key Laboratory of Dynamic Geodesy of CAS, China (No. L09-01); R&I Team Support Program and the Graduate Science and Technology Foundation of SDUST, China (No. YCA110403)
摘    要:HY-2卫星是我国第一颗测高卫星,其径向定轨精度要求厘米量级,搭载了星载GPS接收机。目前HY-2还处于测试阶段,没有公布观测数据。为了确定基于星载GPS的HY-2精密定轨流程及其定轨精度,本文模拟了HY-2卫星星载GPS观测数据,结果表明HY-2星载GPS天线每个历元至少观测7颗GPS卫星。给出了基于星载GPS的精密定轨流程,分别采用简化动力学方法和动态几何法进行了精密定轨实验。对于相位1mm和3mm随机误差的相位观测数据,简化动力学法和动态几何法定轨都能够实现厘米量级的径向精密定轨,几何法定轨精度略低于简化动力定轨。地球重力场模型是影响HY-2卫星精密定轨的重要因素,本文对不同阶次的重力场模型EIGEN2、EGM96、TEG4和GEMT3进行了简化动力学定轨实验,高于50阶次的重力场模型都能够实现厘米级径向精密定轨,主要原因在于大量的高精度星载GPS观测数据和重力场模型精度的提高。

关 键 词:HY-2卫星  星载GPS  精密定轨  简化动力学法  动态几何法

On simulation of precise orbit determination of HY-2 with centimeter precision based on satellite-borne GPS technique
Jin-Yun Guo,Jian Qin,Qiao-Li Kong,Guo-Wei Li.On simulation of precise orbit determination of HY-2 with centimeter precision based on satellite-borne GPS technique[J].Applied Geophysics,2012,9(1):95-107.
Authors:Jin-Yun Guo  Jian Qin  Qiao-Li Kong  Guo-Wei Li
Institution:1. College of Geodesy and Geomatics, Shandong University of Science and Technology, Qingdao, 266590, China
2. Key Laboratory of Surveying and Mapping Technology on Island and Reef of NASMG, Qingdao, 266590, China
Abstract:The HY-2 satellite carrying a satellite-borne GPS receiver is the first Chinese radar altimeter satellite, whose radial orbit determination precision must reach the centimeter level. Now HY-2 is in the test phase so that the observations are not openly released. In order to study the precise orbit determination precision and procedure for HY-2 based on the satellite-borne GPS technique, the satellite-borne GPS data are simulated in this paper. The HY-2 satellite-borne GPS antenna can receive at least seven GPS satellites each epoch, which can validate the GPS receiver and antenna design. What’s more, the precise orbit determination processing flow is given and precise orbit determination experiments are conducted using the HY-2-borne GPS data with both the reduced-dynamic method and the kinematic geometry method. With the 1 and 3 mm phase data random errors, the radial orbit determination precision can achieve the centimeter level using these two methods and the kinematic orbit accuracy is slightly lower than that of the reduced-dynamic orbit. The earth gravity field model is an important factor which seriously affects the precise orbit determination of altimeter satellites. The reduced-dynamic orbit determination experiments are made with different earth gravity field models, such as EIGEN2, EGM96, TEG4, and GEMT3. Using a large number of high precision satellite-borne GPS data, the HY-2 precise orbit determination can reach the centimeter level with commonly used earth gravity field models up to above 50 degrees and orders.
Keywords:HY-2 satellite  satellite-borne GPS technique  precise orbit determination  reduced-dynamic method  kinematic geometry method
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