自主导航星座旋转误差的差分校正技术

孟繁智; 史鹏亮; 欧钢

doi:10.13700/j.bh.1001-5965.2013.0544

自主导航星座旋转误差的差分校正技术

doi: 10.13700/j.bh.1001-5965.2013.0544

1. 国防科技大学电子科学与工程学院, 长沙 410073;
2. 中国人民解放军95899部队, 北京 100085

基金项目:

中国第二代卫星导航系统重大专项资助项目（GFZX0301020211）

详细信息

作者简介:
孟繁智（1981-），男，辽宁盖州人，工程师，mfz9942046@163.com.

中图分类号: TN967.1
计量
- 文章访问数: 1290
- HTML全文浏览量: 51
- PDF下载量: 570
- 被引次数: 0
出版历程
- 收稿日期: 2013-09-24
- 网络出版日期: 2014-08-20

Differential correction technique to the rotation error in autonomous navigation constellation

1. College of Electronic Science and Engineering, National University of Defense Technology, Changsha 410073, China
2. Unit 95899 of PLA, Beijing 100085, China

摘要

摘要: 基于星间观测的自主导航星座存在整体旋转不可测问题，一旦星座发生整体旋转，将导致地面用户定位结果存在偏差.针对这一问题建立了地面用户定位误差模型，运用定位原理和球坐标系变换，从数学上推导了星座整体旋转偏差和地面用户定位偏差之间的关系，在此基础上提出了基于差分原理的旋转误差校正技术，并给出了系统组成和校正算法.使用Walker 12/3/1星座的仿真表明，导航星座旋转误差将导致地面用户的大地经度出现相同角度的偏差，地面用户使用差分校正技术后可有效校正这一误差，在星座整体旋转误差小于1'（相当于赤道地区31 m的水平误差）的条件下，地面用户经差分校正后的水平误差小于 1.5 m，高程误差小于0.003 m.
- 自主导航 /
- 差分校正 /
- 旋转误差 /
- 大地经度 /
- 升交点赤经
Abstract: The rotation of the autonomous navigation constellation is unobservable while using inter-satellite measurements only. Once the rotation occurs, errors will be introduced to the positioning results of ground users. The positioning error model of ground users was established to solve this problem. According to the positioning principle and spherical coordinates transformation, the relationship was mathematically proved between the rotation error of the constellation and the positioning error of ground users. Based on this relationship, a differential correction technique to the rotation error was proposed, including the structure and correction algorithm of the technique. Simulations of the Walker 12/3/1 constellation indicate that the constellation's rotation error will cause the longitude of the ground user to have the same error. After applying the differential correction technique, the ground users will effectively correct this error. While the rotation error is less than 1'(equivalent to a 31 m horizontal error in the equator), the user's horizontal error is less than 1.5 m and the vertical error is less than 0.003 m after differential correcting.
- autonomous navigation /
- differential correction /
- rotation error /
- geodetic longitude /
- longitude of ascending node

HTML全文

参考文献(15)

[1]	Ananda M P, Bernstein H,Cunningham K E,et al.Global positioning system (GPS) autonomous navigation[C]//IEEE Position Location and Navigation Symposium.Piscataway,NJ:IEEE,1990:497-508
[2]	Rajan J A. Highlights of GPS Ⅱ-R autonomous navigation[C]//Proceedings of the 58th Annual Meeting of The Institute of Navigation and CIGTF 21st Guidance Test Symposium.Manassas,VA:The Institute of Navigation,2002:354-363
[3]	刘林,刘迎春. 关于星-星相对测量自主定轨中的亏秩问题[J].飞行器测控学报,2000,19(3):13-16 Liu Lin,Liu Yingchun.Rank deficient problem of inter-satellite measurement in autonomous orbit determination[J].Journal of Spacecraft TT&C Technology,2000,19(3):13-16(in Chinese)
[4]	陈金平,尤政, 焦文海.基于星间距离和方向观测的导航卫星自主定轨研究[J].宇航学报,2005,26(1):43-46 Chen Jinping,You Zheng,Jiao Wenhai.Research on autonav of navigation satellite constellation based on crosslink range and inter-satellites orientation observation[J].Journal of Astronautics,2005,26(1):43-46(in Chinese)
[5]	韩健,董绪荣,杨龙. 星间测向在提高星座自主性中的应用[J].装备指挥技术学院学报,2006,17(1):56-59 Han Jian,Dong Xurong,Yang Long.Application of crosslink orientation observation on increasing autonomy of constellation[J].Journal of the Academy of Equipment Command & Technology,2006,17(1):56-59(in Chinese)
[6]	尚琳,刘国华,刘善伍. 利用分步Kalman滤波器的自主定轨信息融合算法[J].宇航学报,2013,34(3):333-339 Shang Lin,Liu Guohua,Liu Shanwu.An information fusion algorithm of autonomous orbit determination based-on step Kalman filter[J].Journal of Astronautics,2013,34(3):333-339(in Chinese)
[7]	Shang L, Liu G H,Zhang R,et al.An information fusion algorithm for integrated autonomous orbit determination of navigation satellites[J].Acta Astronautica,2013,85:33-40
[8]	朱俊,陈忠贵,廖瑛. 基于脉冲星观测的导航星座自主导航数据融合方法[J].国防科技大学学报,2010,32(4):19-24 Zhu Jun,Chen Zhonggui,Liao Ying.A data fusion method for navigation constellation autonomous navigation based on X-ray pulsar[J].Journal of National University of Defense Technology,2010,32(4):19-24(in Chinese)
[9]	Wei E H, Jin S G,Zhang Q,et al.Autonomous navigation of Mars probe using X-ray pulsars:modeling and results[J].Advances in Space Research,2013,51(5):849-857
[10]	Woodfork D W. Use of X-ray pulsars for aiding GPS satellite orbit determination[D]. Wright-Patterson AFB:Air Force Institute of Technology,2005:2.1-2.34
[11]	Motta S, D'Aì A,Papitto A,et al.X-ray bursts and burst oscillations from the slowly spinning X-ray pulsar IGR J17480-2446 (Terzan 5)[J]. Monthly Notices of the Royal Astronomical Society,2011,414(2):1508-1516
[12]	Qian H M, Sun L,Cai J N,et al.A starlight refraction scheme with single star sensor used in autonomous satellite navigation system[J].Acta Astronautica,2014,96:45-52
[13]	Liu L, Zhang L,Zheng X,et al.Current situation and development trends of star sensor technology[J].Infrared and Laser Engineering,2007(z2):529-533
[14]	Braff R. Description of the FAA's local area augmentation system(LAAS)[J].Journal of the Institute of Navigation,1997,44(4):411-424
[15]	Bertiger W I, Bar-Sever Y E,Haines B J,et al.A real-time wide area differential GPS system[J].Journal of the Institute of Navigation,1997,44(4):433-448