基于航空器载体的卫星定向接收机研究与设计
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- 英文论文题名：Research and Design of Satellite Orientation Receiver Applied to Aircraft
- 论文作者：李立功
- 英文论文作者：Li Ligong ; AVIC Flight Automatic Control Research Institute ; Xi'an
- 年：2016
- 作者机构：中航工业西安飞行自动控制研究所;
- 论文关键词：卫星导航 ; 卫星定向技术 ; 载波相位 ; 卫星接收机
- 英文论文关键词：satellite navigation ; satellite orientation technology ; carrier phase ; satellite receiver
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（上册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：TN967.1
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：4
- 文件大小：538k
- 原文格式：O
- 会议级别：全国
摘要
本文首先介绍了卫星定向技术的发展、原理和关键技术。然后,以一款卫星定向模块为例,从射频单元、基带处理单元、电源模块、数字接口等方面介绍了其硬件设计方案。同时,从数据采集、基带处理算法、导航解算等方面介绍了软件设计方案。最后,本文通过试验验证,证明了该款卫星定向模块的功能及性能均满足航空器载体的应用背景。
Firstly,the development,principle and key technology of Satellite Orientation Technology is presented in this paper.Secondly,we introduce the hardware design scheme included radio frequency unit,baseband processing unit,power unit and digital interface unit.And then the software design scheme is also in troduced,which includes data collection,baseband processing algorithm and navigational resolving.Finally,the satellite orientation unit is proved effective in aircraft through the static test and dynamic test.
Firstly,the development,principle and key technology of Satellite Orientation Technology is presented in this paper.Secondly,we introduce the hardware design scheme included radio frequency unit,baseband processing unit,power unit and digital interface unit.And then the software design scheme is also in troduced,which includes data collection,baseband processing algorithm and navigational resolving.Finally,the satellite orientation unit is proved effective in aircraft through the static test and dynamic test.
引文
[1]吴美平,胡小平,逯亮清,等.卫星定向技术[M].北京:国防工业出版社.2013.
[2]崔建勇.基于卫星导航系统的定向技术研究[D].郑州:解放军信息工程大学,2008.
[3]Spinney V W.Application of Global Positioning System as an Attitude Reference for Near Earth Users[C].ION National Aerospace Meeting,Naval Air Development Center,Warminster,1976.
[4]Richani D Jurgens,Charles E Rodgers,and Leopold C Fan.GPS Azimuth Determining System(ADS)Cycle Resolution,System Design,and Army Test Results[C].National Technical Meeting Proceedings of ION,Sheraton San Marcos Resort Hotel,Phoenix,AZ,1991.
[5]刘子杨.基于GPS的车载定位定向系统研究[D].南京:南京理工大学。2013.
[6]罗治松.基于DSP的GPS定位定向接收机设计[D].南京:南京理工大学,2006.
[7]刘永彪.基于GPS双天线的定向研究[D].南昌:南昌大学,2011.
[2]崔建勇.基于卫星导航系统的定向技术研究[D].郑州:解放军信息工程大学,2008.
[3]Spinney V W.Application of Global Positioning System as an Attitude Reference for Near Earth Users[C].ION National Aerospace Meeting,Naval Air Development Center,Warminster,1976.
[4]Richani D Jurgens,Charles E Rodgers,and Leopold C Fan.GPS Azimuth Determining System(ADS)Cycle Resolution,System Design,and Army Test Results[C].National Technical Meeting Proceedings of ION,Sheraton San Marcos Resort Hotel,Phoenix,AZ,1991.
[5]刘子杨.基于GPS的车载定位定向系统研究[D].南京:南京理工大学。2013.
[6]罗治松.基于DSP的GPS定位定向接收机设计[D].南京:南京理工大学,2006.
[7]刘永彪.基于GPS双天线的定向研究[D].南昌:南昌大学,2011.