期刊文献+

基于GNSS的高轨卫星定位技术研究 被引量:31

Research on Positioning of High Earth Orbital Satellite Using GNSS
下载PDF
导出
摘要 利用全球卫星导航系统(GNSS)进行导航定位具有全球、全天候、实时和高精度的优点,应用于高地球轨道(HEO)卫星的定位,能够提供精确的轨道和姿态确定,并且可以克服目前主要利用地面测控系统对HEO卫星进行定位的设备复杂、投资高等缺点,使得自主导航成为可能.本文对利用GNSS的高轨卫星定位相关技术进行了研究,分析了单一GNSS系统和多个GNSS组合系统的卫星可见性、动态性和几何精度因子(GDOP).通过仿真分析表明,利用组合GNSS系统并通过提高GNSS接收机灵敏度的方法,可以解决GNSS进行HEO卫星定位的相关问题,并能保证HEO卫星定位精度的要求. The GNSS as a navigation and positioning method has global, all-weather, real time and high precision characteristics. Using it on the high earth orbital satellites in positioning can provide precise orbit and attitude determination, overcome the disadvantage of complex equipment and high cost which using ground measurement and control system to positioning, make it possible to autonomous navigation. New and exciting opportunities become possible if satellites are able to autonomously determine their own orbit. For example, precise onboard orbit determination opens the door to satellites flying in formation. However, receivers in low Earth orbit have virtually the same view of the navigation satellite constellation as receivers on the ground. But satellites orbiting at geostationary altitudes and higher have a severely limited view of the main beams of the GNSS satellites. The main beams are either directed away from these high-altitude satellites or they blocked to a large extent by the Earth. So, using much weaker signals is a fundamental requirement for a high orbital altitude GNSS receiver, but it is certainly not the only challenge. Other unique characteristic of this application must also be considered. On the one hand, dynamic characteristics will be more different at high Earth orbit. High dynamic situation makes it difficult to use weaker signals. On the other hand, Position Dilution of Precision (PDOP) figures are much more higher at geostationary and higher altitudes because visible navigation satellites are concentrated in a much smaller region with respect to the spacecraft antenna. Spacecraft navigation receiver must be designed to withstand a variety of extreme environmental conditions. In this paper, positioning of high earth orbital satellites using GNSS is researched. The visibility of navigation satellites, dynamic characteristics, Geometric dilution of precision are analyzed using single GNSS and integrated GNSS. Through simulation and analyzing, it is verified that using GNSS can realize the positioning of HEO satellite and obtain enough positioning precision requirement.
出处 《空间科学学报》 CAS CSCD 北大核心 2008年第4期316-325,共10页 Chinese Journal of Space Science
关键词 全球卫星导航系统 高轨地球卫星 可见性 动态性 几何精度因子 Global Navigation Satellite System (GNSS), High Earth Orbital (HEO) Satellite, Visibility, Dynamic, Geometric Dilution of Precision (GDOP)
  • 相关文献

参考文献10

  • 1杜兰 ,郑勇 ,王宏 ,张云飞 .地球静止卫星精密测定轨技术的现状及发展[J].飞行器测控学报,2005,24(6):14-18. 被引量:12
  • 2Balbach O et al. Tracking GPS above GPS satellite altitude: first results of the GPS experiment on the HEO mission equator-S. In: Position Location and Navigation Symposium, IEEE, Palm Springs, CA, USA, 1998. 243-249.
  • 3Powell T D et al. GPS signals in a geosynchronous transfer orbit: falcon gold data processing. In: Proceedings of Institute of Navigation National Technical Meeting, California, 1999. 575-585.
  • 4Kronman J D et al. Experience using GPS for orbit determination of a geosynchronous satellite, In: Proceedings of the Institute of Navigation GPS 2000 Conference, Salt Lake City: 2000, 1622-1626.
  • 5Michael C et al. Results from the GPS flight experiment on the high earth orbit AMSAT OSCAR-40 spacecraft. In: Proceedings of the Institute of Navigation GPS 2002 Conference, Oregon. 2002, 122-133.
  • 6William Bamford, Luke Winternitz, Curtis Hay. Spacecraft Navigator-Autonomous GPS Positioning at High Earth Orbits. GPS WORLD, 2006.
  • 7孙宝祥,黎涌,高益军.GPS自主定姿定轨技术在新一代大型静止轨道卫星上的应用[J].航天控制,1999,17(3):20-25. 被引量:8
  • 8刘海颖,王惠南.基于GPS的中、高轨道航天器定轨研究[J].空间科学学报,2005,25(4):293-297. 被引量:11
  • 9Parkinson B W, Spilker J J. Global Positioning System: Theory and Applications Volume I. Washington: American Institute of Aeronautics and Astronautics, 1996. 234-242.
  • 10Nesreen I Z. GNSS Receivers for Weak Signals. London: Artech House Books, 2006. 23-32.

二级参考文献22

  • 1Chao C C,Journal of Guidance Control Dynamics,1994年,17卷,4期
  • 2Moreau M C. GPS receiver architecture for autonomous navigation in high earth orbits. Ph.D. Dissertation, Department of Aerospace Engineering Sciences, University of Coloradoat Boulder, 2001
  • 3Laurichesse D et al. Use of GNSS-Based pseudoacceleration measurement and orbital constraints to initialize spaceborne receiver orbit solution. Navigation,2003, 50(2):95-101
  • 4Tsui J B Y. Fundamentals of Global Positioning System Receivers. A Software Approach. New York: Wiley & Sons, 2000, 133-164
  • 5Akos D M et al. Low power global navigation satellite system (GNSS). Signal Detection and Processing. In:Proc. ION GPS 2000. Salt Lake City, UT, 2000, 784-791
  • 6ErikMattiasSoop.地球静止轨道手册[M].北京:国防工业出版社,1999..
  • 7Yunck T P, Wu S C.Ultra-precise orbit determination by GPS.1983, AAS Paper: 83-315.
  • 8Haines B,Lichten S,Srinivasan J,et al. GPS-Like Tracking (GLT) of Geosynchronous Satellites Orbit Determination Results for TDRS. 1995.
  • 9Ward, Douglas T. Operational Improvements of Tracking and Data Relay Satellite (TDRS) Postmaneuver Solutions. Flight Mechanics Symposium, Greenbelt, MD, United States, 2003.
  • 10杜兰 郑勇 王宏.基于测距网/VLBI的 GEO卫星精密定轨[C]..2004航天测控技术研讨会论文集[C].,2004.268-274.

共引文献26

同被引文献218

引证文献31

二级引证文献210

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部