标题: | 利用CHAMP GPS资料决定卫星轨道及地球重力模型 Orbit and gravity model determinations form |
作者: | 许淑珍 Shu-Chen Hsu 黄金维 Cheinway Hwang 土木工程学系 |
关键字: | 地球重力场模型;卫星轨道;CHAMP GPS phase data;gravity model;CHAMP orbit |
公开日期: | 2003 |
摘要: | 本论文结合GPS Prep.和GEODYN II由GPS相位资料采用动力法解算CHAMP轨道,求得之轨道与GFZ公布之CHAMP精密轨道于X、Y、Z三方向的差异量分别为1.454m、3.467m、2.925m,整体而言解算轨道的精度为公尺量级。地球重力场模型是采取两步法利用德国Muenchen技术大学所提供之CHAMP轨道来进行求解,所得之重力场模型称为NCTU,其中以GRACE卫星数据所得之重力场模型GGM01S当做真值,分别减去EGM96和NCTU得到大地起伏差异量、重力异常差异量,结果不管于大地起伏亦或重力异常皆显示所解算的NCTU比EGM96更接近真值,证明了本文所解算的NCTU相较于EGM96其精度确实有改善。时变研究利用一年之CHAMP轨道,每个月选取三天共12组轨道资料,分别以低阶的5阶、10阶重力场模型来看 、 的变化与地心运动,两个阶次的 、 时间变化图形相似,皆有趋近季节性变化,但以10阶的图形较平滑;而地心运动时变图形显示5阶和10阶之1阶球谐系数曲线走势差异性不大。 With the CHAMP GPS phase data, GPS Prep. and GEODYN II are used in a dynamic method to compute CHAMP satellite orbits. The RMS differences in the X, Y, and Z directions between the computed orbits and the GFZ precise orbits are 1.454 m, 3.467 m, 2.925 m, respectively. In general, the accuracy of the computed orbits in this work is at the meter level. A two-step method with data from the Muenchen technical university of Germany is also used to calculate CHAMP satellite orbits and to estimate the earth’s gravity fields. The resulting gravity models are named NCTU models. Both geoid undulations and gravity anomalies from the NCTU models agree better with those from the GGM01S gravity model than those from the EGM96 model. This shows that the NCTU models outperform EGM96. Using one year of CHAMP satellite’s orbital data in a degree-5 solution and a degree-10 solution, the time-variations of J2, J3 and geocenter motions are obtained. The time-variations of J2 and J3 show secular and seasonal variations. The difference in geocenter motion from the degree-5 and degree-10 solutions is marginal. |
URI: | http://140.113.39.130/cdrfb3/record/nctu/#GT009116578 http://hdl.handle.net/11536/49180 |
显示于类别: | Thesis |
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