期刊文献+

GNSS姿态测量接收机性能分析 被引量:2

Analysis on performance of GNSS attitude determination receiver
下载PDF
导出
摘要 利用同源射频平台实现了一种全球导航卫星系统(GNSS)姿态测量的接收机,接收机各射频电路相同且使用同一个晶振驱动,各射频通路之间有相同的信号处理特性。可以将射频通路分为主射频通路和从射频通路,主射频通路实现信号的捕获与跟踪,从射频通路利用差分相位鉴别器完成测量观测量提取。与传统使用独立接收机实现载波差分测向不同,主射频通道进入跟踪状态后立即输出观测量,无需检测载波半周跳变,实现快速姿态测量。利用GNSS姿态测量接收机、Novatel接收机以及惯性导航系统进行了跑车实验,实验结果表明:姿态测量接收机具有更好的载波测量输出能力,姿态测量精度和商业接收机相当。 A global navigation satellite system( GNSS) attitude determination receiver is implemented using homologous RF platform,each RF circuit of the receiver is the same and is driven by the same one crystal oscillator,so each RF access has same character of signal processing. RF access can be divided into Master RF signal path and Slaver RF signal path,and master RF signal path completes acquisition and tracking task and the Slaver RF signal path deals with measurements extraction. Different from traditional independent receiver,observed quantity is output at the same time that Master RF access entering tracking state,no detection of half-cycle slips is needed,fast attitude measurements is realized. Dynamic experiment is carried out where the GNSS attitude determination receiver,Novatel receiver and the INS are mounted on a car,and experimental results show that the receiver has a better carrier measurement and output capacity,and the precision of attitude measurement is the same as commercial receiver.
出处 《传感器与微系统》 CSCD 2015年第2期65-68,72,共5页 Transducer and Microsystem Technologies
关键词 全球导航卫星系统 姿态测量 同源射频平台 载波相位测量 整周模糊度 global navigation satellite system(GNSS) attitude determination homologous RF platform carrier phase measurement integer ambiguity
  • 相关文献

参考文献7

  • 1Parkinson B W, Jr J J S. Global positioning system:Theory and application [ M ]. 2nd ed, Washington, DC : American Institute of Aeronautics and Astronautics, Inc,2006.
  • 2Clark Emerson Cohen. Attitude determination using GPS [ D ]. Stanford : Stanford University, 1992.
  • 3Keong J H. GPS/GLONASS attitude determina-tion with a com- mon clock using a single difference approach [ C ]//Proceedings of ION-GPS, 1999 : 14 -17.
  • 4Teunissen P .l G. Least-squares estimation of the integer GPS am- biguities[ C ]//Invited lecture, section IV : theory and methodolo- gy, IAG General Meeting, Beijing, China, 1993.
  • 5Buist P. The baseline constrained LAMBDA method tbr single epoch, sine frequency attitude determination applications [ C ]// Proceedings of the 20th International Technical Meeting of the Satellite Division of The Institute of Navigation ( ION GNSS 2007 ) ,2001:2962 -2973.
  • 6Bishop G, Welch G. An introduction to the Kalman filter[J]. Proe of SIGGRAPH, Course ,2001,8:27599 -3175.
  • 7Fujikawa S J,Zimbehnan D F. Spacecraft atti-tude determination by Kalman filtering of global positioning system signals [J]. Jour- nal of Guidance, Control, and Dynamics, 1995,18 ( 6 ) : 1365 - 1371.

同被引文献23

引证文献2

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