@inproceedings{7807f95149e74d4d9ab7bf3daaa8d7a5,
title = "Adaptive output feedback tracking control for 6 DOF spacecraft formation flying under actuator faults",
abstract = "This paper studies the output feedback tracking control for 6 degree-of-freedom (DOF) spacecraft formation flying (SFF) subject to system uncertainties, input constraints and actuator faults. A pseudo-velocity filter is designed, and the adaptive neural network (NN) technique is employed to approximate unknown dynamics. A low-cost fault tolerant part is included in the controller to compensate the actuator faults. It is shown that the tracking errors are uniform ultimate bounded (UUB) under the derived controller. Simulation results are given to show the effectiveness of the proposed method.",
keywords = "6 degree-of-freedom, Spacecraft formation flying, actuator faults, input constraints, neural network, output feedback",
author = "Lin Zhao and Yingmin Jia and Wei Huo and Changqing Chen",
note = "Publisher Copyright: {\textcopyright} 2015 IEEE.; 27th Chinese Control and Decision Conference, CCDC 2015 ; Conference date: 23-05-2015 Through 25-05-2015",
year = "2015",
month = jul,
day = "17",
doi = "10.1109/CCDC.2015.7162305",
language = "英语",
series = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "2303--2308",
booktitle = "Proceedings of the 2015 27th Chinese Control and Decision Conference, CCDC 2015",
address = "美国",
}