TY - JOUR
T1 - Event-model-based fuzzy sliding mode deployment control for triangular tethered satellite systems suffering external disturbance
AU - Huang, Bingxiao
AU - Zhang, Fan
AU - Song, Mengshi
AU - Huang, Panfeng
N1 - Publisher Copyright:
© 2023 Elsevier Masson SAS
PY - 2023/8
Y1 - 2023/8
N2 - This paper researches the deployment control problem of the space triangular tethered satellite system under external disturbances and communication constraints from sensor to controller. An adaptive model-based event-triggered fuzzy sliding mode control scheme is proposed, making sure that the system is deployed to the specified configuration. The disturbance observer is used to estimate external disturbances, while the estimated model is constructed at the controller side to update control input without interruption under event-triggered mechanism. Then, the event-triggered fuzzy sliding mode controller based on the estimated model is designed, ensuring that the communication burden is greatly reduced and precise deployment control is achieved. Further, the stability of the closed-loop system is proved by the Lyapunov function based on the hybrid dynamical system. Eventually, the effectiveness of the proposed control scheme is tested by simulation tests.
AB - This paper researches the deployment control problem of the space triangular tethered satellite system under external disturbances and communication constraints from sensor to controller. An adaptive model-based event-triggered fuzzy sliding mode control scheme is proposed, making sure that the system is deployed to the specified configuration. The disturbance observer is used to estimate external disturbances, while the estimated model is constructed at the controller side to update control input without interruption under event-triggered mechanism. Then, the event-triggered fuzzy sliding mode controller based on the estimated model is designed, ensuring that the communication burden is greatly reduced and precise deployment control is achieved. Further, the stability of the closed-loop system is proved by the Lyapunov function based on the hybrid dynamical system. Eventually, the effectiveness of the proposed control scheme is tested by simulation tests.
KW - Disturbance observer
KW - Fuzzy sliding mode control
KW - Hybrid dynamical system
KW - Model-based event-triggered control
KW - Space tethered system
UR - http://www.scopus.com/inward/record.url?scp=85159859126&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2023.108399
DO - 10.1016/j.ast.2023.108399
M3 - 文章
AN - SCOPUS:85159859126
SN - 1270-9638
VL - 139
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 108399
ER -