Orbit Design for Approaching Multiple Space Objects in a Circular Orbit

摘要：

　　This paper focuses on orbit design for a spacecraft without orbital maneuver approaching multiple objects in a circular orbit.Based on the assumption of no perturbation,a series of relations of approach orbit elements and geocentric angle between objects are established by theory analysis and formula derivation.Then characteristics of approach orbit are derived from a large number of data and numerical analysis.Finally a simulation example with Earth Geostationary Orbit as target circular is shown.

关键词： Without maneuver Circular orbit Approaching orbit Orbit design

作者: WEI Yanyan WANG Hongyu LV Zhaofu

作者单位: Army Aviation Institute,Beijing,101123,China 65529Army,Liaoyang,111000,China

会议类型: 国际会议

会议名称: 2014 Asia-Pacific International Symposium on Aerospace Technology(2014亚太航空航天技术学术会议)

会议地点: 上海

会议语种:英文

页码: 1-7

在线出版日期: 2014-09-24（万方平台首次上网日期，不代表论文的发表时间）