期刊文献+

分布式航天器间距离测量信号处理机的设计 被引量:1

Design of Distributed Spacecraft System Autonomous Relative Ranging Signal Processor
下载PDF
导出
摘要 根据分布式航天器小型化要求,采用大容量可编程门阵列(field programmable gate array,FPGA)和数字信号处理器(DSP)设计了一种分布式航天器间距离测量信号处理机,处理机可以对航天器间的相对距离进行高精度测量,实现航天器自主距离解算;根据距离测量对处理机的设计要求,从硬件结构和软件模块设计上讨论了处理机的设计思想和方法;最后在处理机上进行了航天器间相对距离测量模拟试验,证明了处理机的宽带信号处理能力。 According to miniaturization requirement of distributed spacecraft, a distributed space-craft relative ranging processor is designed using high capacity field programmable gate array (FPGA) and digital signal processing(DSP). The ranging processor can high precisely accomplish relative distance measurement and realize calculation of autonomous relative ranging between spacecrafts. According to design requirement of distance measurement, design scheme and technique of processor is discussed based on hardware structure and software module. Finally simulation of distributed space-craft relative ranging is applied on processor, and simulation result proved processor having wideband processing capacity.
出处 《装备指挥技术学院学报》 2008年第1期60-64,共5页 Journal of the Academy of Equipment Command & Technology
关键词 分布式航天器 软件无线电 可编程门阵列 伪码测距 distributed spacecraft software radio field programmable gate array(FPGA) pseu-do code ranging
  • 相关文献

参考文献9

  • 1WU Senchong, KUANG Da. Positioning with autonomous formation flyer on space technology[C]// ION GPS. 12^th inernational technical meeting of the satellite division of the institute of navigation. Nashville : ION GPS]. 1999 : 14-17.
  • 2KONG E, MILLER D, SEDWICK R. Optimal trajectories and orbit design for separated spacecraft interferometry[D]. Boston:Thesis of Degree of Master of Science at the Massachusetts Institute of Technology, 1998 : 35-39.
  • 3杏建军,郗晓宁,王威,高玉东.星间相对测量在三星编队中的应用[J].空间科学学报,2003,23(4):286-293. 被引量:11
  • 4TIEN J Y,SRINICASAN J M, YOUNG J E. Formation acquisition sensor for the terrestrial planet finder(TPF) mission[J]. IEEE Aerospace Conference Proceedings,2004,6 (2) :2680-2690.
  • 5HIROBUMI S,TATSNAKI H, KENJI K. Micro-scanning laser range finders and position-attitude determination for formation flight[C]//AIAA. 13^th Annual AIAA/USU conference on small Satellites. New Mexico:AIAA,1999:82-87.
  • 6REED J H, Software radio: A modern approach to radio engineering [M]. New York: Prentice Hall PTR, 2001: 234-270.
  • 7ALTERA CORPORATION. NiosⅡ processor reference handbook[EB/OL]. (2004-12-5)[2005-2-5]. http://www.altera. com/documents/nios. html.
  • 8Kaplan,E.D.邱致和,王万义译.GPS原理与应用[M].北京:电子工业出版社,2002.
  • 9马宏,王元钦.基于扩频技术的相对距离自主测量方法研究[J].宇航学报,2005,26(1):29-33. 被引量:7

二级参考文献11

  • 1ElliottDKaplan著 邱致和 王万义译.GPS原理与应用[M].北京:电子工业出版社,2002..
  • 2Purcell G, Kuang D, Lichten S, Wu S, Young L. Autonomous formation flyer sensor technology development. Paper AAS 98-062, 21st Ann. AAS Guid. Cont. Conf., Breckenridge, 1998. 1--21.
  • 3Park Chan-Woo, How Jonathan P, Capots Larry. Sensing technologies for formation flying spacecraft in LEO using CDGPS and an inter-spacecraft communications system. ION GPS 2000, 2000, Salt Lake City, 1595---1607.
  • 4Wu Sien-Chong, Kuang Da. Positioning with Autonomous Formation Flyer (AFF) on Space-Technology 3. ION GPS'99, 1999, Nashville, 385---392.
  • 5Parkinson B W, Spilker J J Jr et al. Global Positioning System: Theory and Applications. Prog.Astron. Aeron., Amer. Ins. Aeron. Astron., Inc., 1996.
  • 6Olsen E A, Park Chan-Woo, How Jonathan P. Carrier-phase bias initialization for formation flying vehicles with onboard pseudolites. ION GPS'99, 1999, Nashville, 459--468.
  • 7Bauer F,Bristow J,Folta D,Hartman K,Quinn D,How J P.Satellite formation flying using an innovative autonomous control system(AUTOCON)enviroment[A]. In:proceedings of the AIAA GNC Conf[C],(New Orieana,LA),May 1997
  • 8查光明 熊贤祚.扩频通信[M].西安:西安电子科大出版社,1999.158.
  • 9王忠,黄顺吉.扩频测距系统中多径跟踪误差研究[J].系统工程与电子技术,1999,21(7):37-40. 被引量:5
  • 10孙宏伟,李志刚,李焕信,梁双友.卫星双向时间比对原理及比对误差估算[J].宇航计测技术,2001,21(2):55-58. 被引量:30

共引文献40

同被引文献7

引证文献1

二级引证文献4

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