Satellite Formation Flying using Low Thrusters and Solar Sail

摘要：

　　An automatic formation flying control using low thrusters is proposed in this paper.To use continuous thrusters,dynamics of orbit elements are derived based on Gauss variational equations.To reduce the fuel consumption and compose the formation in more efficient way,Solar sail is suggested as a support actuator.The cone/clock angles of the sail normal vector are given by a least square approach.

关键词： Satellite Formation Flying Relative Orbit Element Vectors Solar Sail

作者: Yeerang Lima Hyochoong Banga

作者单位: Aerospace Engineering Department,KAIST,291 Daehak-ro,Yuseong-gu,Daejeon,305-701,South Korea

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: 1-5

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）