Event- and self-triggered control of attitude coordination to multi-spacecraft system

被引:16
|
作者
Zhang, Chengxi [1 ]
Wu, Jin [2 ]
Dai, Ming-Zhe [3 ]
Li, Bo [4 ]
Wang, Mingjiang [1 ]
机构
[1] Harbin Inst Technol, Sch Elect & Informat Engn, Shenzhen, Peoples R China
[2] Hong Kong Univ Sci & Technol, Dept Elect & Comp Engn, Hong Kong, Peoples R China
[3] Cent South Univ, Sch Aeronaut & Astronaut, Changsha, Peoples R China
[4] Shanghai Maritime Univ, Inst Logist Sci & Engn, Shanghai, Peoples R China
来源
关键词
Attitude consensus; Event-triggered control; Self-triggered control; Multi-spacecraft; RIGID SPACECRAFT; SYNCHRONIZATION; STABILIZATION; TRACKING; DESIGN;
D O I
10.1108/AEAT-02-2020-0037
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Purpose The purpose of this paper is to investigate the attitude cooperation control of multi-spacecraft with in-continuous communication. Design/methodology/approach A decentralized state-irrelevant event-triggered control policy is proposed to reduce control updating frequency and further achieve in-continuous communication by introducing a self-triggered mechanism. Findings Each spacecraft transmits data independently, without the requirement for the whole system to communicate simultaneously. The local predictions and self-triggered mechanism avoid continuous monitoring of the triggering condition. Research limitations/implications This investigation is suitable for small Euler angle conditions. Practical implications The control policy based on event-triggered communication can provide potential solutions for saving communication resources. Originality/value This investigation uses event- and self-triggered policy to achieve in-communication for the multi-spacecraft system.
引用
收藏
页码:1085 / 1092
页数:8
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