含钟差修正的脉冲星和太阳观测组合导航

杨成伟; 邓新坪; 郑建华; 高东

含钟差修正的脉冲星和太阳观测组合导航

1.
中国科学院研究生院, 北京 100190
2. 中国科学院空间科学与应用研究中心, 北京 100190

基金项目: 空间科学预先研究资助项目(XDA04074300)

详细信息

中图分类号: V448.224
计量
- 文章访问数: 1579
- HTML全文浏览量: 4
- PDF下载量: 666
- 被引次数: 0
出版历程
- 收稿日期: 2011-07-22
- 网络出版日期: 2012-11-30

Integrated navigation based on pulsars and sun observation including clock error correction

1.
Graduate University of Chinese Academy of Sciences, Beijing 100190, China
2. Center for Space Science and Applied Research,Chinese Academy of Sciences, Beijing 100190, China

摘要

摘要: 为提高深空探测器巡航段的导航定位精度和钟差修正能力,提出一种利用X射线脉冲星和太阳观测信息的组合导航方法.利用脉冲星导航的脉冲到达时间测量值,同时利用太阳敏感器、分光计分别测量太阳视线矢量和探测器相对于太阳的径向速度,并将星载时钟钟差增广为状态变量,构建组合导航系统,利用基于扩展卡尔曼滤波的UD(Upper triangular matrix-Diagonal matrix)分解信息融合算法进行状态估计.仿真结果表明,该方法能有效解决因钟差漂移引起的导航滤波发散问题,同脉冲星导航相比,该方法提高了定位精度和钟差修正能力.
- 脉冲星 /
- 太阳观测 /
- 组合导航 /
- 钟差修正 /
- UD分解
Abstract: In order to improve the accuracy of navigation and clock correction of a deep space probe during cruise phase, an integrated navigation method was advanced. By combining the X-ray pulsar based navigation(XPNAV) with the sun line-of-sight vector, and the radial velocity of the probe relative to the sun, an integrated navigation system was advanced by using information fusion, based on extended kalman filter(EKF). The state of atomic clock error was considered in the system model. The UD factorization algorithm was applied to control the rounding error. The simulation results demonstrate that this method can control the divergence rendered by the clock error in EKF. Compared with XPNAV, this method can provide a higher navigation precision and more effectively control the clock error.
- pulsars /
- sun observation /
- integrated navigation /
- clock error correction /
- UD factorization

HTML全文

参考文献(10)

[1]	叶培建,彭兢.深空探测与我国深空探测展望[J].中国工程科学,2006,8(10):13-18 Ye Peijian,Peng Jing.Deep space exploration and its prospect in China [J].Engineering Science,2006,8(10):13-18(in Chinese)
[2]	Riedel J E,Bhaskaran S,Desai S,et al.Autonomous optical navigation (AutoNav) DS1 technology validation report [R].JPL Publication 00-10,2000
[3]	Sheikh S I.The use of variable celestial X-ray sources for spacecraft navigation.Maryland:Department of Aerospace Engineering,University of Maryland,2005
[4]	Sheikh S I,Pines D J.Recursive estimation of spacecraft position and velocity using X-ray pulsar time of arrival measurements[J].Navigation,2006,53(3):149-166
[5]	Guo Y P.Self-contained autonomous navigation system for deep space missions [J].Advances in the Astronautical Sciences,1999,102(2):1099-1113
[6]	Yim J R,Crassidis J L,Junkins J L.Autonomous orbit navigation of interplanetary spacecraft [C]//AIAA/AAS Astrodynamics Specialist Conference.Denver,CO:AIAA,2000:53-61
[7]	Woodfork D W.The use of X-ray pulsars for aiding GPS satellite orbit determination.Alabama:Department of the Air Force,Air University,2005
[8]	付梦印,邓志红,闫莉萍.Kalman滤波理论及其在导航系统中的应用[M].北京:科学出版社,2010:78-79 Fu Mengyin,Deng Zhihong,Yan Liping.Theory and application of Kalman filter in navigation system [M].Beijing:Science Press,2010:78-79(in Chinese)
[9]	向政,富立,范跃祖.L-D分解求逆法在联邦卡尔曼滤波中的应用[J].北京航空航天大学学报,2003,29(8):749-752 Xiang Zheng,Fu Li,Fan Yuezu.Application of L-D factorization in calculating inverse in federated filer [J].Journal of Beijing University of Aeronautics and Astronautics,2003,29(8):749-752(in Chinese)
[10]	谢振华,许录平,倪广仁.基于最大似然的X射线脉冲星空间定位研究[J].宇航学报,2007,28(6):1605-1608 Xie Zhenhua,Xu Luping,Ni Guangren.X-ray pulsars-based spacecrafts- position determination algorithm based on maximum likelihood estimation [J].Journal of Astronautics,2007,28(6):1605-1608(in Chinese)