Analysis and Design of the Automatic Flight Dynamics Operations For Geostationary Satellite Mission

被引:2
|
作者
Lee, Byoung-Sun [1 ]
Hwang, Yoola [1 ]
Park, Sangwook [2 ]
Lee, Young-Ran [2 ]
Noguero Galilea, Javier Santiago [3 ]
机构
[1] ETRI, Satellite Control & Nav Res Team, Daejeon 305700, South Korea
[2] Satrec Initiat, Aerosp Syst Team, Daejeon 305811, South Korea
[3] GMV Aerosp & Def SA, E-28760 Madrid, Spain
关键词
satellite orbit; flight dynamics; mission control; automation; COMS;
D O I
10.5140/JASS.2009.26.2.267
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
Automation of the key flight dynamics operations for the geostationary orbit satellite mission is analyzed and designed. The automation includes satellite orbit determination, orbit prediction, event prediction, and fuel accounting. An object-oriented analysis and design methodology is used for design of the automation system. Automation scenarios are investigated first and then the scenarios are allocated to use cases. Sequences of the use cases are diagramed. Then software components and graphical user interfaces are designed for automation. The automation will be applied to the Communication, Ocean, and Meteorology Satellite (COMS) flight dynamics system for daily routine operations.
引用
收藏
页码:267 / 278
页数:12
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