Structural analogy for control of satellite formations

被引:0
作者
Avanzini, Giulio [1 ]
de Matteis, Guido [2 ]
Tarantini, Valerio [2 ]
机构
[1] Politecn Torino, Dept Aerosp Engn, Corso Duca Abruzzi 24, I-10129 Turin, Italy
[2] Univ Roma La Sapienza, Dept Mech & Aeronaut, I-00184 Rome, Italy
来源
ASTRODYNAMICS 2005, VOL 123, PTS 1-3 | 2006年 / 123卷
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The application of the structural analogy to the control of a formation of satellites is discussed and a novel control system architecture is presented. The main contribution of the paper is the integration of two techniques for control of systems of multiple agents/vehicles, namely, the formation feedback control and the node augmentation technique. Development of the latter technique is carried out to generate maneuvers in a three-dimensional space. Performance of the proposed control algorithm is demonstrated by numerical simulations of the closed-loop system. A figure of merit that quantifies the deformation of the formation graph is defined in order to compare the results with those obtained with an existing, single-level control algorithm.
引用
收藏
页码:399 / +
页数:3
相关论文
共 10 条
  • [1] [Anonymous], 2002, AIAA GUID NAV CONTR
  • [2] BEARD RW, 2001, IEEE T CONTROL SYSTE, V9
  • [3] Eren T, 2002, IEEE DECIS CONTR P, P2959, DOI 10.1109/CDC.2002.1184306
  • [4] High precision formation control of mobile robots using virtual structures
    Lewis, MA
    Tan, KH
    [J]. AUTONOMOUS ROBOTS, 1997, 4 (04) : 387 - 403
  • [5] OLFATISABER R, 2002, UNPUB IEEE C DEC CON
  • [6] OLFATISABER R, IEEE C DEC CONTR
  • [7] OLFATISABER R, 2002, 15 IFAC WORLD C JUN
  • [8] OLFATISABER R, 2002, IEEE C DEC CONTR LAS
  • [9] Decentralized scheme for spacecraft formation flying via the virtual structure approach
    Ren, W
    Beard, RW
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2004, 27 (01) : 73 - 82
  • [10] REN W, 2004, REV SUBMISSION IEEE