@inproceedings{f6648e2e5d7c489f80500b6fa43d4586,
title = "Orbital and Attitude Cooperative Control of Formation Flying Small Satellite",
abstract = "This paper is concerned with orbital and attitude cooperative control problems of small satellite in formation flying operation. At first, positional and attitude error dynamics model of small satellite relative to a target satellite is derived. Then, considering the uncertain inertia matrix and mass of small satellite, we design an adaptive output feedback control law and its stability is proved. Finally, numerical simulation validate the performance of the proposed output feedback control strategy.",
keywords = "adaptive control, formation flying, output feedback, small satellite",
author = "Yang Jia and Yan Jie",
note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 2nd IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference, IMCEC 2018 ; Conference date: 25-05-2018 Through 27-05-2018",
year = "2018",
month = sep,
day = "20",
doi = "10.1109/IMCEC.2018.8469741",
language = "英语",
series = "Proceedings of 2018 2nd IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference, IMCEC 2018",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1735--1738",
editor = "Bing Xu",
booktitle = "Proceedings of 2018 2nd IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference, IMCEC 2018",
}