TY - GEN
T1 - Decentralized Fixed-Time Attitude Synchronization Control for Spacecraft Formation Flying
AU - Sui, Weishun
AU - Duan, Guang Ren
AU - Zhang, Maorui
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8
Y1 - 2018/8
N2 - In this paper, the decentralized fixed-time attitude synchronization problem is considered for multiple rigid spacecraft system. A multispacecraft fixed-time-based terminal sliding mode is designed, which possesses the predefined convergence time independent of initial condition. Then, the decentralized attitude control laws by employing the fixed-time-based terminal sliding mode are proposed, which can avoid the singularity and guarantee the attitude tracking errors converge to zero in fixed time. Finally, numerical simulations are presented to demonstrate the performance of the new controllers.
AB - In this paper, the decentralized fixed-time attitude synchronization problem is considered for multiple rigid spacecraft system. A multispacecraft fixed-time-based terminal sliding mode is designed, which possesses the predefined convergence time independent of initial condition. Then, the decentralized attitude control laws by employing the fixed-time-based terminal sliding mode are proposed, which can avoid the singularity and guarantee the attitude tracking errors converge to zero in fixed time. Finally, numerical simulations are presented to demonstrate the performance of the new controllers.
UR - https://www.scopus.com/pages/publications/85082441131
U2 - 10.1109/GNCC42960.2018.9019075
DO - 10.1109/GNCC42960.2018.9019075
M3 - 会议稿件
AN - SCOPUS:85082441131
T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Y2 - 10 August 2018 through 12 August 2018
ER -