@inproceedings{d8b6d0d5065148899c9c5aef119f9efc,
title = "Attitude Consensus of Multiple Uncertain Spacecraft Systems with Sensor Faults and Input Delay",
abstract = "This paper studies multi-spacecraft system attitude consensus control with model uncertainty, sensor faults and time-varying input delay. Attitude dynamics of the spacecraft is described using Euler angles. Predictor-based state transformation method is proposed to get delay-free system states with delay information unknown. Afterwards, descriptor observer is used to estimate system states and sensor disturbances. Disturbance attenuation controller is designed based on system state estimates. Finally, a simulation example demonstrates the system performance under the designed algorithm.",
keywords = "Attitude consensus, Input delay, Multi-spacecraft system, Sensor faults",
author = "Yunhan Li and Xing Xin and Chunyan Wang and Keyu Zheng",
note = "Publisher Copyright: {\textcopyright} The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2025.; International Conference on Guidance, Navigation and Control, ICGNC 2024 ; Conference date: 09-08-2024 Through 11-08-2024",
year = "2025",
doi = "10.1007/978-981-96-2212-2\_1",
language = "English",
isbn = "9789819622115",
series = "Lecture Notes in Electrical Engineering",
publisher = "Springer Science and Business Media Deutschland GmbH",
pages = "1--10",
editor = "Liang Yan and Haibin Duan and Yimin Deng",
booktitle = "Advances in Guidance, Navigation and Control - Proceedings of 2024 International Conference on Guidance, Navigation and Control Volume 4",
address = "Germany",
}