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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, PP. 1033-1037

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Abstract:

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Walker12/3/1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31m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1.5m,高程误差小于0.003m.

References

[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

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