TY - JOUR
T1 - Attitude Coordination Control for Spacecraft with Disturbances and Event-Triggered Communication
AU - Wang, Chenliang
AU - Guo, Lei
AU - Wen, Changyun
AU - Yu, Xiang
AU - Huang, Jian
N1 - Publisher Copyright:
© 1965-2011 IEEE.
PY - 2021/2
Y1 - 2021/2
N2 - In this article, a novel distributed attitude coordination control scheme is proposed for a group of rigid spacecraft with unknown disturbances. The communication topology is described by a general directed graph, and the leader's attitude is available to only a small fraction of followers. Different from existing attitude coordination control schemes, here an event-triggered communication strategy without Zeno phenomenon is designed, which avoids continuous communication between neighboring spacecraft and considerably reduces the communication burden. Moreover, a nonlinear observer is constructed for each follower, which enables us to estimate and compensate for a large class of disturbances exactly. The proposed scheme is able to ensure the boundedness of all closed-loop signals and steer the attitude tracking errors into an arbitrarily small residual set, regardless of the intermittent communication. Simulation results illustrate the effectiveness of the proposed scheme.
AB - In this article, a novel distributed attitude coordination control scheme is proposed for a group of rigid spacecraft with unknown disturbances. The communication topology is described by a general directed graph, and the leader's attitude is available to only a small fraction of followers. Different from existing attitude coordination control schemes, here an event-triggered communication strategy without Zeno phenomenon is designed, which avoids continuous communication between neighboring spacecraft and considerably reduces the communication burden. Moreover, a nonlinear observer is constructed for each follower, which enables us to estimate and compensate for a large class of disturbances exactly. The proposed scheme is able to ensure the boundedness of all closed-loop signals and steer the attitude tracking errors into an arbitrarily small residual set, regardless of the intermittent communication. Simulation results illustrate the effectiveness of the proposed scheme.
KW - Attitude control
KW - distributed coordination
KW - disturbance observer
KW - event-triggered communication
KW - spacecraft
UR - https://www.scopus.com/pages/publications/85101457767
U2 - 10.1109/TAES.2020.3027408
DO - 10.1109/TAES.2020.3027408
M3 - 文章
AN - SCOPUS:85101457767
SN - 0018-9251
VL - 57
SP - 586
EP - 596
JO - IEEE Transactions on Aerospace and Electronic Systems
JF - IEEE Transactions on Aerospace and Electronic Systems
IS - 1
M1 - 9209098
ER -