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地球重力场模型对低轨卫星轨道积分的影响
引用本文:周建,吕志伟. 地球重力场模型对低轨卫星轨道积分的影响[J]. 测绘工程, 2012, 21(2): 14-16. DOI: 10.3969/j.issn.1006-7949.2012.02.004
作者姓名:周建  吕志伟
作者单位:1.中国卫星海上测控部,江苏江阴,214431;2.信息工程大学测绘学院,河南郑州,450052
摘    要:
介绍3种不同的地球重力场模型及其(约化)动力学定轨中所涉及的动力学模型,并基于Collocation轨道积分方法对CHAMP卫星进行数值积分,然后将轨道积分结果与JPL快速精密星历相比较.实验结果表明,由CHAMP卫星SST数据反演生成的EIGEN-2模型引力位系数具有较高的精度,能够满足低轨卫星精密定轨的需要.

关 键 词:重力场模型  低轨卫星  轨道积分  EIGEN-

The effects of earth's gravity field models to LEO orbit integration
ZHOU Jian , LV Zhi-wei. The effects of earth's gravity field models to LEO orbit integration[J]. Engineering of Surveying and Mapping, 2012, 21(2): 14-16. DOI: 10.3969/j.issn.1006-7949.2012.02.004
Authors:ZHOU Jian    LV Zhi-wei
Affiliation:1.China Satellite Maritime Tracking and Control Department,Jiangyin 214431,China;2.Institute of Surveying and Mapping,Information Engineering University,Zhengzhou 450052,China)
Abstract:
Firstly,the paper introduces three different gravity field models for LEO satellites and the dynamical models in reduced-dynamic or dynamic orbit determination,then it is possible to compare the orbit integration results to JPL rapid precise orbit.All the results indicate that the EIGEN-2 model coefficients which was produced by CHAMP SST data has higher precision and that model can meet the needs of precise orbit determination of LEO satellites.
Keywords:gravity field models  LEO satellites  orbit integration  EIGEN-2
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