| 电子式飞行仪表系统与GPS导航系统交联关系设计与实现 |
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| 引用本文： | 唐金元,于潞,张鹏明.电子式飞行仪表系统与GPS导航系统交联关系设计与实现[J].飞机设计,2008,28(2):67-70. |
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| 作者姓名： | 唐金元 于潞 张鹏明 |
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| 作者单位： | 海军航空工程学院,青岛分院,山东,青岛,266041 |
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| 摘 要： | 在简要分析某型飞机上原装LTN-211奥米加导航系统与EFIS-74电子式飞机仪表系统交联特性和Trimble 2101I／0型GPS导航系统输出特性基础上，设计了该型机LTN-211换装Trimble 2101I／O后EFIS-74与Trimble 2101I／O新的交联关系。实际应用表明：所实现的EFIS-74与Trimble 2101I／O交联关系全面、正确，提高了该型飞机的整机导航能力。
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| 关 键 词： | 电子式飞行仪表系统 GPS 导航系统 交联 设计 |
Designing and Realizing of Airborne EFIS and GPS Navigation System Interfacing Methods |
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| TANG Jin-yuan,YU Lu,ZHANG Peng-ming.Designing and Realizing of Airborne EFIS and GPS Navigation System Interfacing Methods[J].Aircraft Design,2008,28(2):67-70. |
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| Authors: | TANG Jin-yuan YU Lu ZHANG Peng-ming |
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| Institution: | TANG Jin-yuan, YU Lu, ZHANG Peng-ming ( Qingdao Branch of Naval Aeronautical Engineering Institute, Qingdao 266041, China) |
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| Abstract: | Based on briefly introducing about interfacing characteristics between LTN-211 OMEGA long range navigation system and EFIS-74 electronic flight instrument system installed in one carrier aircraft and output characteristics of Trimble 2101 I/O approach GPS navigation system,this paper analyzes interfacing methods between EFIS-74 and Trimble 2101I/O,which replaces LTN-211.Actual applying shows that the interfacing methods designed between EFIS-74 and Trimble 2101 I/O are complete and correct,enhancing the whole navigation abilities of the carrier aircraft. |
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| Keywords: | electronic flight instrument system(EFIS) GPS navigation system interfacing designing |
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