@inproceedings{87503df188244721be84504820fa8144,
title = "Distributed Adaptive Full Order Sliding Mode Control for Attitude Synchronization of Rigid Spacecraft",
abstract = "This paper investigates the distributed attitude tracking problem of multiple spacecraft with unknown external disturbances and inertia uncertainties when the time varying reference signal is available to only a subset of group members. Modified Rodriguez parameters are used for attitude representation. The external disturbances and inertia uncertainties are recast into the lumped uncertainties with unknown firstorder derivative upper bound. An adaptive law is proposed to estimate this upper bound. Based on this adaptive law, a distributed adaptive full order sliding mode controller is proposed to achieve attitude synchronization. Simulation results are presented to demonstrate the validity of proposed results.",
author = "Huan Meng and Zhuoyue Song and Nsubuga Latifu and Kai Yan and Qinghe Wu and Xiangdong Liu",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 15th IEEE International Conference on Control and Automation, ICCA 2019 ; Conference date: 16-07-2019 Through 19-07-2019",
year = "2019",
month = jul,
doi = "10.1109/ICCA.2019.8899553",
language = "English",
series = "IEEE International Conference on Control and Automation, ICCA",
publisher = "IEEE Computer Society",
pages = "887--892",
booktitle = "2019 IEEE 15th International Conference on Control and Automation, ICCA 2019",
address = "United States",
}