@inproceedings{77c477d5315f464ba8d90d8920e19a2a,
title = "Magnetic attitude control of bias momentum spacecraft by bounded linear feedback",
abstract = "This paper addresses the three-axis magnetic attitude control of small spacecraft with momentum bias configuration by bounded linear feedback. Necessary and sufficient conditions are derived to guarantee that the linearized dynamics and kinematics are stable in the Lyapunov sense. Explicit solutions to some Lyapunov equations associated with the considered open-loop system are obtained. Based on the explicit solutions to the Lyapunov equation, an explicit saturated linear state feedback controller is designed. Globally asymptotic stability of the closed-loop systems is proved by constructing the explicit Lyapunov function. Simulations show the effectiveness of the proposed approach.",
keywords = "Attitude stabilization, Bounded feedback, Lyapunov equation, Lyapunov stable, Magnetic torque",
author = "Weiwei Luo and Bin Zhou",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 29th Chinese Control and Decision Conference, CCDC 2017 ; Conference date: 28-05-2017 Through 30-05-2017",
year = "2017",
month = jul,
day = "12",
doi = "10.1109/CCDC.2017.7979188",
language = "英语",
series = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "3933--3938",
booktitle = "Proceedings of the 29th Chinese Control and Decision Conference, CCDC 2017",
address = "美国",
}