Decentralized adaptive control for attitude synchronization of multiple spacecraft via quantized information exchange

被引:28
作者
Wu, Baolin [1 ]
Xu, Chuang [1 ]
Zhang, Yingchun [1 ]
机构
[1] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150080, Peoples R China
基金
中国国家自然科学基金;
关键词
Adaptive control; Attitude synchronization; Logarithmic quantizer; Limited communication bandwidth; SLIDING-MODE CONTROL; COORDINATION CONTROL; TRACKING CONTROL; CONSENSUS; TIME;
D O I
10.1016/j.actaastro.2020.05.013
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper investigates the problem of decentralized attitude synchronization and tracking for a group of spacecraft, whose communication topology is undirected, subject to inter-spacecraft communication resources constraints, model uncertainties and external disturbances. In order to reduce inter-spacecraft communication burden, a quantization mechanism is developed. In the quantization mechanism, the quantized sequences, whose storage size are much smaller than that of spacecraft's attitude information, are required to be transmitted among spacecraft only when the quantized sequences changes compared with the previous one. Thus, the size of inter-spacecraft communication data can be greatly reduced. A decentralized adaptive attitude synchronization and tracking control scheme is proposed to align spacecraft's attitude and track the desired attitude. By resorting to Barbalat's Lemma, the resulting closed-loop system is proved to be uniformly ultimately bounded stable. Finally, numerical simulation results are presented to demonstrate the effectiveness of the theoretical results.
引用
收藏
页码:57 / 65
页数:9
相关论文
共 36 条
[1]   Rigid body attitude coordination without inertial frame information [J].
Bai, He ;
Arcak, Murat ;
Wen, John T. .
AUTOMATICA, 2008, 44 (12) :3170-3175
[2]   A coordination architecture for spacecraft formation control [J].
Beard, RW ;
Lawton, J ;
Hadaegh, FY .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2001, 9 (06) :777-790
[3]   Leader-following attitude consensus of multiple rigid body systems by attitude feedback control [J].
Cai, He ;
Huang, Jie .
AUTOMATICA, 2016, 69 :87-92
[4]   The leader-following attitude control of multiple rigid spacecraft systems [J].
Cai, He ;
Huang, Jie .
AUTOMATICA, 2014, 50 (04) :1109-1115
[5]   Predictive Smooth Variable Structure Filter for Attitude Synchronization Estimation During Satellite Formation Flying [J].
Cao, Lu ;
Chen, Yongqiang ;
Zhang, Zhidong ;
Li, Hengnian ;
Misra, Arun K. .
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2017, 53 (03) :1375-1383
[6]   Optimal Open-Loop Control for 2-D Colloid Transport in the Dead-End Microchannel [J].
Chen, Tehuan ;
Zhou, Shichao ;
Ren, Zhigang ;
Xu, Chao .
IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2019, 27 (06) :2757-2765
[7]   Rotation-Matrix-Based Attitude Tracking for Multiple Flexible Spacecraft with Actuator Faults [J].
Chen, Ti ;
Shan, Jinjun .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2019, 42 (01) :181-188
[8]   Distributed attitude synchronization of formation flying via consensus-based virtual structure [J].
Cong, Bing-Long ;
Liu, Xiang-Dong ;
Chen, Zhen .
ACTA ASTRONAUTICA, 2011, 68 (11-12) :1973-1986
[9]  
DeVille L., 2016, OPTIMIZING GERSHGORI
[10]   Leader-follower cooperative attitude control of multiple rigid bodies [J].
Dimarogonas, Dimos V. ;
Tsiotras, Panagiotis ;
Kyriakopoulos, Kostas J. .
SYSTEMS & CONTROL LETTERS, 2009, 58 (06) :429-435