Impact of Atmospheric Coupling Between Orbit and Attitude in Relative Dynamics Observability

被引:5
作者
Chaves-Jimenez, Adolfo [1 ]
Guo, Jian [1 ]
Gill, Eberhard [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Kluyverweg 1, NL-2629 HS Delft, Netherlands
关键词
STATE ESTIMATION; SPACECRAFT; POSITION; TRANSLATION; SATELLITES; SYSTEM; MISSIONS; ROTATION;
D O I
10.2514/1.G002618
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:3273 / +
页数:8
相关论文
共 40 条
[1]  
Alfriend K., 2009, SPACECRAFT FORMATION, V2
[2]  
Alfriend K. T., 2002, 2002 AIAA AAS ASTR S
[3]  
[Anonymous], 2011, International Journal of Control and Automation
[4]  
[Anonymous], 2010, THESIS
[5]   A novel unscented predictive filter for relative position and attitude estimation of satellite formation [J].
Cao, Lu ;
Chen, Xiaoqian ;
Misra, Arun K. .
ACTA ASTRONAUTICA, 2015, 112 :140-157
[6]   TERMINAL GUIDANCE SYSTEM FOR SATELLITE RENDEZVOUS [J].
CLOHESSY, WH ;
WILTSHIRE, RS .
JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (09) :653-&
[7]  
D'Amico S, 2005, ADV ASTRONAUT SCI, V120, P831
[8]  
Dullerud G. E., 2013, COURSE ROBUST CONTRO, V36
[9]  
Gaulocher S., 2005, AIAA GUID NAV CONTR
[10]   Formation flying within a constellation of nano-satellites: The QB50 mission [J].
Gill, E. ;
Sundaramoorthy, P. ;
Bouwmeester, J. ;
Zandbergen, B. ;
Reinhard, R. .
ACTA ASTRONAUTICA, 2013, 82 (01) :110-117