Solar radiation pressure used for formation flying control around the Sun-Earth libration point

被引:0
作者
龚胜平
李俊峰
宝音贺西
机构
[1] SchoolofAerospace,TsinghuaUniversity
关键词
solar sail; solar radiation pressure; halo orbit; formation flying;
D O I
暂无
中图分类号
V448.2 [航天器制导与控制];
学科分类号
081105 ;
摘要
Solar radiation pressure is used to control the formation flying around the L2 libration point in the Sun-Earth system. Formation flying control around a halo orbit requires a very small thrust that cannot be satisfied by the latest thrusters. The key contribution of this paper is that the continuous low thrust is produced by solar radiation pressure to achieve the tight formation flying around the libration point. However, only certain families of formation types can be controlled by solar radiation pressure since the direction of solar radiation pressure is restricted to a certain range. Two types of feasible formations using solar radiation pressure control are designed. The conditions of feasible formations are given analytically. Simulations are presented for each case, and the results show that the formations are well controlled by solar radiation pressure.
引用
收藏
页码:1009 / 1016
页数:8
相关论文
共 12 条
[1]  
Fundamental motions near collinear libra-tion points and their transitions. Barden B T,Howell K C. Journal of the Astronautical Sci-ences . 1998
[2]  
Formation flying with decentral-ized control in libration point orbits. Folta D,Carpenter J R,Wagner C. International Symposium:Spaceflight Dynamics . 2000
[3]  
Formation flying satellite control around the L2 Sun-Earth libration point. Hamilton N H. . 2001
[4]  
A Non-linear approach to spacecraft for-mation control in the vicinity of a collinear libration point. Luquette R J,Sanner R M. Proceedings of the AAS/AIAA Astrodynamics Specialists Conference . 2001
[5]  
Stabilizing and specifying motion relative to unstable tra-jectories:applications to spacecraft formation flight. Hsiao F Y. . 2004
[6]  
Adaptive Neural Control of Deep-space Formation Flying. Pini Gurfil,Moshe Idan,N Jeremy Kasdin. Proceedings of the American Control Conference . 2002
[7]  
Dynamics and control of spacecraft formationflying in three-body trajectories. Gurfil P,,Kasdin N J. Proceedings of the AIAA Guid-ance,Navigation,and Control Conference and Exhibit . 2001
[8]  
Spacecraft formation keeping near the libration points of the Sun.Earth/Moon system. Marchand B G. . 2004
[9]  
Orbit Determination Error Analysis and Station-Keeping for Libration Point Trajectories. Gordon,S.Graig. . 1991
[10]  
Trajectory design and stationkeeping formultiple spacecraft in formation near the Sun-Earth L1 point. Howell K C,Barden B T. Proceedings of the 50th IAF International Astronautical Congress . 1999