THE CONDITIONAL EQUATION AND ITS WEIGHTING COEFFICIENTS OF THE DIFFERENTIAL ORBIT IMPOROVEMENT USING CONCENTRATED DATA OF THE DIRECTION OBSERVATION

Abstract

Abstract: Making the use of the fact that the rate of the direction observation can be obtained with aid of the information of concentrated data of the direction observation, in this paper a new method of improving the orbit determination, is presented, which can set up the conditional equations of both the direction observation and its rate simultaneously, and calculate their weighting coefficients as well. The method is believed to be useful for some practical and routine work to improve the accuracy of the orbit determination.

Key words: Direction finding, Orbit determination, Calculation method.

Lu Benkui, Rong Pengzhi (Purple Mountain Observatory, Academia Sinica). THE CONDITIONAL EQUATION AND ITS WEIGHTING COEFFICIENTS OF THE DIFFERENTIAL ORBIT IMPOROVEMENT USING CONCENTRATED DATA OF THE DIRECTION OBSERVATION[J]. .

[1]	WANG Da-Bao, WANG Zhong-Guo, TANG Hai-Tao, CAO Jing. GPS Based Orbit Determination Algorithm with High Precisionand Low Computational Complexity for LEO Remote Sensing Satellites [J]. , 2014, 34(2): 54-61.
[2]	GUO Xiang, ZHANG Qiang, ZHAO Qi-Le, GUO Jing. Precise Orbit Determination for LEO Satellites Using Single-frequency GPS Observations [J]. , 2013, 33(2): 41-46.
[3]	CHEN Zhi-Guo, CHEN Pei, HAN Chao. Algorithm for Ground-base Orbit Determination of Navigation Satellites [J]. , 2012, 32(3): 27-34.
[4]	LIU Wen-Xiang, MOU Wei-Hua, WANG Fei-Xue. Effect Analysis of Measuring Time Error on Single Satellite Orbit Determination Error [J]. , 2011, 31(4): 70-76.
[5]	LI Dong, YI Dong-Yun, CHENG Hong-Wei. Orbit Determination for GEO Objects with Short Arcs ofSpaceBased Optical Observations [J]. , 2011, 31(3): 1-7.
[6]	LIU Li, DONG Xu-Rong, ZHENG Kun, WANG Wei. Integral Filter Method of Orbit Determination for Geostationary Satellite Based on Spaceborne GNSS [J]. , 2011, 31(1): 70-75.
[7]	LIU Guang-Ming, LIAO Ying, CHEN Zhong-Gui. Initial Orbit Determination with Space-based Angle Measurements Based on General Regularization Least Squares Estimation [J]. , 2010, 30(04): 1-8.
[8]	Wang Hui Gu Xuemai (Harbin Institute of Technology,Harbin 150001). Autonomous Relative Orbit Determination for Satellite Formation Flying [J]. , 2009, 29(03): 50-56+63.
[9]	Jiang Weinan Zhou Haiyin Duan Xiaojun Pan Xiaogang(Science College,National University of Defense Technology,Changsha 410073). Self-adaptive Selecting Method for Scaling Factor of Scaled Unscented Transformation [J]. , 2008, 28(03): 1-6+28.
[10]	Pan Xiaogang Zhou Haiyin(Department of Mathematic and System Science,National University of Defense Technology,Changsha 410073). Research on Method of Spacecraft Orbit Determination Based on Penalized Least Squares Estimation [J]. , 2008, 28(02): 15-20+50.
[11]	Che Rucai Zhang Honghua(Beijing Institute of Control Engineering,Beijing 100080). Investigation of Relative Orbit Determination Method for Tracking a Space Non-cooperative Target [J]. , 2007, 27(04): 7-13.
[12]	Wu Gongyou1 Wang Jiasong2 Zhao Changyin1 Chen Jianrong2(1 Purple Mountain Observatosy,Chinese Academy of Sciences,Nanjing 210008)(2 Xi′an Satellite Control Center,Xi′an 710043). Multiple Satellites Joint Orbit Determination based on Satellite-to-satellite and Satellite-to-earth Tracking [J]. , 2007, 27(03): 58-63.
[13]	Zhu Zhuanmin Xu Zongben(Mathematical College of Xi′an Jiaotong University,Xi′an 710049). Study of Satellite Initial Orbit Determination Method [J]. , 2007, 27(03): 1-6.
[14]	Zhu Zhuanmin~* Qiu Hongxing~(*) Xu Zongben~(Mathematical College of Xi′an Jiaotong University,Xi′an 710049)(*Nanjing Zijinshan Astronomical Observatory of China Academy of Sciences,Nanjing 210008). The Error Estimate to the Single Circle Observation Data of Satellite [J]. , 2005, 25(05): 29-33.
[15]	Wang Jiongqi Wu Yi (National University of Defence Technology, Changsha 410073). An Approach for Moonlet Precise Orbit Determination Based on Satellite Formation Flying [J]. , 2005, 25(03): 8-13.

THE CONDITIONAL EQUATION AND ITS WEIGHTING COEFFICIENTS OF THE DIFFERENTIAL ORBIT IMPOROVEMENT USING CONCENTRATED DATA OF THE DIRECTION OBSERVATION

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