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利用最小二乘直接法反演卫星重力场模型的MPI并行算法 被引量:11
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作者 周浩 罗志才 +1 位作者 钟波 陆飚 《测绘学报》 EI CSCD 北大核心 2015年第8期833-839,857,共8页
针对海量卫星重力数据反演高阶次地球重力场模型的密集型计算任务与高内存耗用问题,基于MPI实现了最小二乘直接法恢复高阶次位系数的并行算法。引入并行读写、分块存储与分块计算等方式完成了设计矩阵的构建、法方程的形成与求解等密集... 针对海量卫星重力数据反演高阶次地球重力场模型的密集型计算任务与高内存耗用问题,基于MPI实现了最小二乘直接法恢复高阶次位系数的并行算法。引入并行读写、分块存储与分块计算等方式完成了设计矩阵的构建、法方程的形成与求解等密集型计算任务的并行算法,数值计算结果表明三者的并行相对效率峰值可分别达到95%、68%、63%。利用GOCE轨道跟踪和径向扰动重力梯度数据(共518 400个历元)分别反演了120、240阶次地球重力场模型,计算时间仅为40min、7h,内存耗用峰值仅为290MB、1.57GB;采用与GOCE同等噪声水平的观测数据恢复的重力场模型精度与GOCE已发布模型的解算精度相一致,联合GRACE和GOCE的解算模型能够实现二者独立信息的频谱互补,表明本文方法可高效稳定地恢复高阶次地球重力场模型。 展开更多
关键词 MPI 并行算法 卫星重力场模型 Gauss-Jordan算法 GOCE
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重力场模型谱组合精化区域似大地水准面
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作者 张衡 朱伟 张省 《测绘科学》 CSCD 北大核心 2023年第4期54-59,共6页
针对区域似大地水准面模型构建中地面重力数据分布不均匀且较难获取的难题,该文提出一种基于谱组合重力场模型的似大地水准面精化方法,实现了卫星重力场模型与高阶重力场模型的优化组合,结合293个实测全球卫星导航系统(GNSS)水准数据,... 针对区域似大地水准面模型构建中地面重力数据分布不均匀且较难获取的难题,该文提出一种基于谱组合重力场模型的似大地水准面精化方法,实现了卫星重力场模型与高阶重力场模型的优化组合,结合293个实测全球卫星导航系统(GNSS)水准数据,构建了山东省范围的高精度似大地水准面模型。利用GNSS水准数据检核表明:在山东省范围,利用谱组合重力场模型构建的区域似大地水准面模型具有较高的精度,能够满足大多数工程要求,与采用地面重力数据构建的似大地水准面模型对比发现,在不使用地面重力数据的情况下也可构建厘米级精度似大地水准面模型,具有成本低、效率高的明显优势,便于及时开展区域似大地水准面的维护更新。 展开更多
关键词 谱组合 卫星重力场模型 似大地水准面 高阶重力场模型
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GOCE kinematic orbit adjustment for EGM validation and accelerometer calibration
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作者 徐天河 孙张振 +2 位作者 江楠 陈康康 李敏 《Journal of Central South University》 SCIE EI CAS 2014年第6期2397-2403,共7页
The main principle and mathematical model of GOCE kinematic orbit adjustment for Earth gravity field model (EGM) validation and accelerometer calibration are presented. Based on 60 days GOCE kinematic orbits with 1-... The main principle and mathematical model of GOCE kinematic orbit adjustment for Earth gravity field model (EGM) validation and accelerometer calibration are presented. Based on 60 days GOCE kinematic orbits with 1-2 cm accuracy and accelerometer data from 2009-11-02 to 2009-12-31, the RMS-of-fit (ROF) of them using EGM2008, EIGEN-SC, ITG- GRACE2010S and GOCO01S up to 120, 150 and 180 degree and order (d/o) are evaluated and compared. The scale factors and biases of GOCE accelerometer data are calibrated and the energy balance method (EBM) is performed to test the accuracy of accelerometer calibration. The results show that GOCE orbits are also sensitive to EGM from 120 to 150 d/o. The ROFs of EGMs with 150 and 180 d/o are obviously better than those of EGMs with 120 d/o. The ROFs of GOCO01S and ITG-GRACE2010S are almost the same up to 120 and 150 d/o, which are about 3.3 cm and 1.8 cm, respectively. They are far better than those of EGM2008 and EIGEN-SC with the same d/o. The ROF of GOCO01S with 180 d/o is about 1.6 em, which is the best one among those EGMs. The accelerometer calibration accuracies (ACAs) of ITG-GRACE2010S and GOCO01S are obviously higher that those of EGM2008 and EIGEN-SC. The ACA of GOCO01S with 180 d/o is far higher than that of EGMs with 120 d/o, and a little higher than that of ITG-GRACE2010S with 150 d/o. I t is suggested that the newest released EGM such as GOCO01S or GOCO02S till at least 150 d/o should be chosen in GOCE precise orbit determination (POD) and accelerometer calibration. 展开更多
关键词 GOCE orbit adjustment Earth gravity field model kinematic orbit accelerometer calibration
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The Chang’E-1 orbiter plays a distinctive role in China’s first successful selenodetic lunar mission 被引量:4
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作者 PING JinSong SU XiaoLi +1 位作者 HUANG Qian YAN JianGuo 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2011年第12期2130-2144,共15页
The first Chinese lunar orbiter Chang'E-1 is a successful mission with many fruitful results obtained in various disciplines. The scientific data acquired by the Chang'E-1 payloads can benefit studies of the l... The first Chinese lunar orbiter Chang'E-1 is a successful mission with many fruitful results obtained in various disciplines. The scientific data acquired by the Chang'E-1 payloads can benefit studies of the lunar origin and evolution, as well as other relevant research areas, after careful validation of the data. Among the new results, the Chang'E-1 selenodetic products are continually uncovering characteristics of the lunar surface, undersurface and inner structure. Successful lunar orbiters such as the Clementine, Lunar Prospector, KAGUYA/SELENE, Chang'E-1, Lunar Reconnaissance Orbiter and GRAIL have been revealing, with increasing clarity, global selenodetic characteristics with state-of-the-art fine resolution and high precision. In particular, the Chang'E-1 plays an important distinctive role in selenodetic exploration through enhancing lunar topography and gravity models. The gravity model has been successfully improved with a factor of two after applying the Chang'E-1 long-wavelength tracking data. Using the new models, some medium-scale lunar surface characteristics such as basins and volcanoes have been identified. Furthermore, the old mascon basins of Bouguer, gravity anomaly and craters have been discovered with the Chang'E-1 selenodetic data. 展开更多
关键词 Chang’E-1 lunar orbiter lunar science selenodesy TOPOGRAPHY GRAVITY
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