Decentralized scheme for spacecraft formation flying via the virtual structure approach

被引:492
作者
Ren, W [1 ]
Beard, RW [1 ]
机构
[1] Brigham Young Univ, Dept Elect & Comp Engn, Provo, UT 84602 USA
关键词
D O I
10.2514/1.9287
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Built on the combined strength of decentralized control and the recently introduced virtual structure approach, a decentralized formation scheme for spacecraft formation flying is presented. Following a decentralized coordination architecture via the virtual structure approach, decentralized formation control strategies are introduced, which are appropriate when a large number of spacecraft are involved and/or stringent interspacecraft communication limitations are exerted. The effectiveness of the proposed control strategies is demonstrated through simulation results.
引用
收藏
页码:73 / 82
页数:10
相关论文
共 31 条
[21]  
Ren W., 2002, 20024963 AIAA
[22]  
ROBERTSON A, 1999, P AM CONTR C SAN DIE
[23]  
Stilwell DJ, 2000, IEEE CONTR SYST MAG, V20, P45, DOI 10.1109/37.887448
[24]  
Sugar T, 1998, IEEE INT CONF ROBOT, P2916, DOI 10.1109/ROBOT.1998.680672
[25]  
Tanner HG, 2002, IEEE DECIS CONTR P, P2439, DOI 10.1109/CDC.2002.1184201
[26]  
Wang PKC, 1996, J ASTRONAUT SCI, V44, P315
[27]   NAVIGATION STRATEGIES FOR MULTIPLE AUTONOMOUS MOBILE ROBOTS MOVING IN FORMATION [J].
WANG, PKC .
JOURNAL OF ROBOTIC SYSTEMS, 1991, 8 (02) :177-195
[28]   THE ATTITUDE-CONTROL PROBLEM [J].
WEN, JTY ;
KREUTZDELGADO, K .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1991, 36 (10) :1148-1162
[29]  
Wertz JR, 1978, SPACECRAFT ATTITUDE
[30]   QUATERNION FEEDBACK REGULATOR FOR SPACECRAFT EIGENAXIS ROTATIONS [J].
WIE, B ;
WEISS, H ;
ARAPOSTATHIS, A .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1989, 12 (03) :375-380