Dynamical decomposition modeling and control of multi-spacecraft coordinated flying

被引:0
|
作者
Astronautics College, Northwest Polytechnical University, Xi'an 710072, China [1 ]
机构
来源
Harbin Gongye Daxue Xuebao | 2009年 / 11卷 / 147-151期
关键词
D O I
暂无
中图分类号
V476.2 [宇宙飞船];
学科分类号
摘要
This paper presents a dynamics modeling and control scheme for multi-spacecraft coordinated flying based on dynamical decomposition. With certain decomposition arithmetics, physically separated spacecrafts can be connected together, and multi-spacecraft coordinated flying involved in complicated motions can be decomposed into two parts, one is the group motion of multi-spacecraft flying and the other is the relative motion of spacecrafts formation flying. The dynamics models of these two subsystems possess the similar form with that of a single spacecraft, and the formation maintenance, reconfiguration and formation transfer within a large scope can be realized by controlling one of the subsystems. Tracking control laws for group system and formation system are also designed, and their stability is proved by Lyapunov theorem. Simulation results validate the effectiveness of the decomposition arithmetics and the control scheme.
引用
收藏
页码:147 / 151
相关论文
共 50 条
  • [21] Multi-spacecraft, trajectory optimization and control using Genetic Algorithm techniques
    Seereeram
    Li
    Ravichandran
    Mehra
    Smith, R
    Beard, R
    2000 IEEE AEROSPACE CONFERENCE PROCEEDINGS, VOL 7, 2000, : 99 - 108
  • [22] Robust attitude consensus control of multi-spacecraft with stochastic link failure
    Zhu Y.
    Kang Z.
    Zhu H.
    Wu S.
    Zhan X.
    Shen Q.
    Zhong C.
    Aerospace Systems, 2023, 6 (04) : 581 - 594
  • [23] Prescribed Performance Rotating Formation Control of Multi-Spacecraft Systems with Uncertainties
    Liu, Yan
    Qin, Kaiyu
    Li, Weihao
    Shi, Mengji
    Lin, Boxian
    Cao, Lu
    DRONES, 2022, 6 (11)
  • [24] Multi-spacecraft observations of earthward flow bursts
    REME Henry
    DANDOURAS Iannis
    DUNLOP Malcolm
    LUCEK Elisabeth
    Science China(Technological Sciences), 2012, (05) : 1305 - 1311
  • [25] On the error estimation of multi-spacecraft timing method
    Zhou, X. -Z.
    Pu, Z. Y.
    Zong, Q. -G.
    Song, P.
    Fu, S. Y.
    Wang, J.
    Zhang, H.
    ANNALES GEOPHYSICAE, 2009, 27 (10) : 3949 - 3955
  • [26] COLLISION-AVOIDANCE AUTONOMOUS CONTROL ALGORITHM FOR MULTI-SPACECRAFT PROXIMITY OPERATIONS
    Xu, Dan-Dan
    Zhang, Jing
    Luo, Ya-Zhong
    FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III, 2018, 165 : 123 - 136
  • [27] Attitude control of multi-spacecraft systems on SO(3) with stochastic links failure
    KANG Zeyu
    SHEN Qiang
    WU Shufan
    Chris J.DAMAREN
    MU Zhongcheng
    Chinese Journal of Aeronautics, 2024, 37 (03) : 320 - 331
  • [28] Decentralized specific tracking control on SE(3) for constrained multi-spacecraft systems
    Zhang, Xiaoxiang
    Geng, Yunhai
    Wu, Baolin
    NONLINEAR DYNAMICS, 2025, 113 (07) : 6757 - 6780
  • [29] Velocity-free attitude coordinated tracking control for spacecraft formation flying
    Hu, Qinglei
    Zhang, Jian
    Zhang, Youmin
    ISA TRANSACTIONS, 2018, 73 : 54 - 65
  • [30] Relative position coordinated control for spacecraft formation flying with obstacle/collision avoidance
    Wenjia Wang
    Chuanjiang Li
    Yanning Guo
    Nonlinear Dynamics, 2021, 104 : 1329 - 1342