首页 | 本学科首页   官方微博 | 高级检索  
     检索      

Simulation of the Impacts of Single LEO Satellite Orbit Parameters on the Distribution and Number of Occultation Events
作者姓名:XU  Xiaohua  LI  Zhenghang  LUO  Jia
作者单位:LI Zhenghang LUO Jia XU Xiaohua,lecturer,Ph.D,Institute of Satellite Application,School of Geodesy and Geomatics,Wuhan University,129 Luoyu Road,Wuhan 430079,China.
基金项目:Funded by the 0pen Research Fund Program of the Key Laboratory of Geospace Environment and Geodesy, Ministry of Education,China (No. 03-04- 09).
摘    要:Introduction WithGPSreceiversmountedonLEOsatel lites,GPSoccultationeventscanbeobserved.Theobservablesarevaluableforatmospheric monitoringandweatherforecasting.Whenpre paringtobuildupanLEOsatelliteoccultation observationsystem,theevaluation,designand imple…

关 键 词:卫星  全球定位系统  GPS  轨道参数
文章编号:1009-5020(2006)01-013-05
收稿时间:2005-09-09

Simulation of the impacts of single LEO satellite orbit parameters on the distribution and number of occultation events
XU Xiaohua LI Zhenghang LUO Jia.Simulation of the Impacts of Single LEO Satellite Orbit Parameters on the Distribution and Number of Occultation Events[J].Geo-Spatial Information Science,2006,9(1):13-17.
Authors:Xu Xiaohua Ph D  Li Zhenghang  Luo Jia
Institution:(1) Institute of Satellite Application, School of Geodesy and Geomatics, Wuhan University, 129 Luoyu Road, 430079 Wuhan, China
Abstract:Focusing on carrying out GPS occultation observat io ns with a receiver set on LEO satellite, this paper develops the LEO orbit simul ation system based on which the occultation events can be simulated taking into account the geometric relationship of the satellites and the field of view of th e receiver antenna. In this paper, the impacts of 4 types of LEO orbit parameter s including argument of latitude (AOL), right ascension of ascending node (RAAN) , orbit height and orbit inclination on the distribution and number of occultati on events observed with a single LEO satellite are discussed through simulat ion and some conclusions are drawn.
Keywords:LEO satellite  GPS  occultation  orbit parameters
本文献已被 CNKI 维普 万方数据 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号