期刊文献+

资源一号02D卫星双频GPS导航系统容错设计 被引量:1

Fault-tolerant Design of Dual-frequency GPS Navigation System for ZY-1-02D Satellite
下载PDF
导出
摘要 资源一号02D卫星采用双频GPS导航系统提高定位精度,而空间环境等因素可能引起双频GPS导航系统在轨短暂非定位,从而影响整星时统及有效载荷的持续成像。为此,文章提出双频GPS导航系统容错设计,从整星层面和单机层面进行定位状态、通信状态、时间状态等自主管理及容错处理。试验验证和在轨验证结果表明:采用容错设计的双频GPS导航系统在出现短时间非定位时处理措施有效,能够保证资源一号02D卫星整星连续正常工作。 The dual-frequency GPS navigation system has been applied to ZY-1-02D satellite to improve the positioning accuracy.However,the space environment may cause temporary non-positioning of dual-frequency GPS navigation system on orbit which can affect the entire satellite’s time-keeping accuracy,thus influencing the payload’s continuous imaging quality.In order to overcome this problem,a fault-tolerant design for the dual-frequency GPS navigation system is proposed in this paper.An autonomous management and fault-tolerant processing mechanism of positioning state,communications state and time state are employed to the dual-frequency GPS navigation system from the system’s and product’s perspectives.The test and on-orbit verification results show that the dual-frequency GPS navigation system with fault-tolerant design can work properly and keep the continuity of the ZY-1-02D entire satellite service while encountering temporary non-positioning situation.
作者 王建 赵里恒 武小栋 胡萍 苏莹 WANG Jian;ZHAO Liheng;WU Xiaodong;HU Ping;SU Ying(Institute of Remote Sensing Satellite, China Academy of Space Technology, Beijing 100094, China;Space Star Technology Co., Ltd., Beijing 100095, China;Xi’an Institute of Space Radio Technology, Xi’an 710071, China;Beijing Research Institute of Telemetry, Beijing 100076, China)
出处 《航天器工程》 CSCD 北大核心 2020年第6期128-135,共8页 Spacecraft Engineering
基金 国家重大航天工程。
关键词 资源一号02D卫星 双频GPS导航系统 多层级 容错设计 服务连续性 ZY-1-02D satellite dual-frequency GPS navigation system multi-layer and multi-level fault-tolerant design service continuity
  • 相关文献

参考文献6

二级参考文献38

  • 1李征航.全球定位系统(GPS)技术新进展:第一讲 AS技术与GPS接收机技术的发展[J].武测科技,1995(4):42-48. 被引量:4
  • 2田明浩,冯永新,潘成胜.一种基于P码的频域直接捕获算法的研究[J].电子学报,2007,35(3):549-552. 被引量:18
  • 3周忠谟 易杰军 周琪.GPS卫星测量原理与应用(修订版)[M].北京:测绘科学出版社,1996.P140~141.
  • 4[2]Bisnath S B,Langley,R B.Precise,efficient GPS-based geometric tracking of low Earth orbiters[R].Institute of Navigation,Annual Meeting,55th,Cambridge,MA,1999:751-760
  • 5[3]Reigber C,Schwintzer P,Neumayer K-H,et al.The CHAMP-only earth gravity field model EIGEN-2[J].Advances in Space Research (0273-1177),2003,31(8):1883-1888
  • 6[4]Beutler G.Earth gravity field from space-From sensors to earth sciences:closing remarks[J].Space Science Reviews,2004,110(4):359-368
  • 7Wilkinson D C, Stone J L, et al. TDRS-1 single event up- sets and the effect of the space environment [ J ]. IEEE Trans. on Nuclear Science, 1991, 38(6) : 1708-1712.
  • 8Underwood C I, Oldfield M K. Observations on the relia- bility of COTS-device-based solid state data recorders op- erating in low-earth orbit [ J ]. IEEE Trans. on Nuclear Science, 2000, 47 (3) : 647- 653.
  • 9Purohit S, Harrington D, Margala M. An area efficient de- sign methodology for SEU tolerant digital circuits [ J ]. Proceedings of 2010 IEEE International Symposium on Circuits and Systems, 2010:981-984.
  • 10Li Hao, Lixin Yu. A study on the hardware implementa- tion of EDAC[ J ]. Third 2008 International Conference on Convergence and Hybrid Information Technology, 2008: 222-225.

共引文献21

同被引文献8

引证文献1

二级引证文献2

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