1. 中国科学院光电研究院
2. 中国科学院研究生院
纸质出版:2012
移动端阅览
[1]周韩雯,刘伟,袁洪,魏东岩.不同INS器件对GNSS/INS深耦合接收机跟踪环路的影响[J].传感器与微系统,2012,31(08):83-86.
ZHOU Han-wen1, LIU Wei1, YUAN Hong1, et al. Effect of different INS devices on GNSS/INS deep-coupled receiver tracking loop[J]. 2012, 31(8): 83-86.
[1]周韩雯,刘伟,袁洪,魏东岩.不同INS器件对GNSS/INS深耦合接收机跟踪环路的影响[J].传感器与微系统,2012,31(08):83-86. DOI: 10.13873/j.1000-97872012.08.017.
ZHOU Han-wen1, LIU Wei1, YUAN Hong1, et al. Effect of different INS devices on GNSS/INS deep-coupled receiver tracking loop[J]. 2012, 31(8): 83-86. DOI: 10.13873/j.1000-97872012.08.017.
针对在GNSS/INS深耦合接收机产品设计中INS器件的选用问题
仿真研究了不同动态条件下
导航级、战术级和商业级这3种不同性能级别的INS器件对GNSS/INS深耦合组合接收机跟踪环路的影响。深耦合组合接收机能较大程度上降低失锁临界带宽
提高载波跟踪精度。导航级、战术级及商业级深耦合接收机在不同动态下的载波环临界带宽可以分别压窄到1~1.8
1.5~2.7 Hz和2~4 Hz;临界带宽下的载波跟踪环的误差分别在19°
22°和27°以内;速度误差分别在0.05~0.5
0.1~1.0
0.2~2.0 m/s。上述结果为GNSS/INS深耦合接收机中的INS器件选型提供了理论依据。
The effect of three different property levels of INS devices
navigation level
tactical level and commercial level
on GNSS/ INS deep-coupled receiver tracking loop is studied under different dynamic conditions for the INS devices selection in deep-coupled receiver.From this
the GNSS/INS deep-coupled receiver can reduce the critical bandwidth of lock-lose to a much greater extent
improve the lock-lose conditions of the traditional receiver and the carrier tracking precision.The critical bandwidthes of the navigation level
tactical level and commercial level deep-coupled receiver are 1~1.8
1.5~2.7Hz
and 2~4Hz
respectively.The carrier tracking errors are less than 19°
22°
and 27°
respectively.The velocity errors are 0.05~0.5
0.1~1.0m/s
and 0.2~2.0m/s
respectively.Above results provide theoretical basis for the INS devices selection in deep-coupled receiver.
SINS辅助GPS跟踪环路超紧耦合系统设计 [J]. 于洁,王新龙. 北京航空航天大学学报 . 2010(05)
超紧密组合下GPS/INS跟踪回路的结构及性能分析 [J]. 高翔,刘兴堂. 战术导弹技术 . 2007(01)
GPS原理与接收机设计[M]. 电子工业出版社 , 谢钢, 2009
惯性导航[M]. 科学出版社 , 秦永元编著, 2006
GPS原理与应用[M]. 电子工业出版社 , [美]ElliottD.Kaplan著, 2002
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