The Mission Design Tool for Hybrid Orbit Satellite Constellation about Configuration Design and Management Strategy

摘要：

In this paper, the platform of design, analysis and simulation for satellite constellation design and control tool (CDT) is developed, to deal with the design issues of the constellation life cycle, including hybrid orbit constellation configuration design, deployment strategy, station-keeping strategy, reconfiguration strategy, reinforcement strategy, and also the convenient manipulation and demonstration interface, which is a genetic tool for the different mission demand and restriction. The tool architecture, processing flow, and run flow are explained detailedly in illustration, with brief correlative literature summary and algorithms presentation. The demonstration experiment about navigation constellation composed of inclined geosynchronous (IGSO), geostationary (GEO), and Medium Earth Orbit (MEO) satellites is carried out and the simulation result satisfies the reliability requirements, which is important to primary mission design for Chinese global navigation satellite system, Beidou-2.

关键词： hybrid orbit constellation configuration design deployment strategy station-keeping strategy reconfiguration strategy reinforcement strategy CDT

作者: Cui Hongzheng Han Chao Wang Shaokai Tang Zhongxing

作者单位: School of Astronautics, Beihang University, BUAABeijing, P. R. China School of Astronautics, Beihang University, BUAA Beijing, P. R. China

会议类型: 国际会议

会议名称: 2010 3rd International Conference on Advanced Computer Theory and Engineering(2010年第三届先进计算机理论与工程国际会议 ICACTE 2010)

会议地点: 成都

会议语种:英文

页码: 1-6

在线出版日期: 2010-08-20（万方平台首次上网日期，不代表论文的发表时间）