@inproceedings{8bc3f70d3230491f96486699c39cb408,
title = "Integrated Attitude-Orbit Control for Spacecraft Proximity Operations Based on Dual Quaternion",
abstract = "This paper studies the tracking control problem of integrated attitude-orbit motion for spacecraft proximity operations. Firstly, the model of the relative integrated attitude-orbit motion between a chaser and a target spacecraft is established in terms of dual quaternion description. An adaptive terminal sliding mode control algorithm is developed to accomplish simultaneous position and attitude tracking control considering external disturbances, uncertainties of mass parameters and unknown actuator faults. The practical finite-time stability of the closed-loop integrated attitude-orbit control system is realized via the presented controller. Finally, numerical simulation is proposed to indicate the validity of the designed control algorithm.",
keywords = "Adaptive Control, Dual Quaternion, Integrated Attitude-Orbit Motion, Spacecraft Proximity Operations",
author = "Qian Sun and Yingmin Jia",
note = "Publisher Copyright: {\textcopyright} 2022 Technical Committee on Control Theory, Chinese Association of Automation.; 41st Chinese Control Conference, CCC 2022 ; Conference date: 25-07-2022 Through 27-07-2022",
year = "2022",
doi = "10.23919/CCC55666.2022.9901657",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3293--3298",
editor = "Zhijun Li and Jian Sun",
booktitle = "Proceedings of the 41st Chinese Control Conference, CCC 2022",
address = "美国",
}