@inproceedings{dff3ce3c62a947fabfa2e5615c495c13,
title = "Modeling and attitude control of a spinning spacecraft with internal moving mass",
abstract = "An attitude control system of a spinning spacecraft with internal moving mass is presented in this paper. This system consists of a rigid body and two internal radial moving masses. The mathematical model, including attitude kinematics and nonlinear dynamics equations, is established based on Newtonian mechanics. The control law is designed based on the linearquadratic- regulator (LQR) theory. The performance of the controller is demonstrated in numerical simulation, and the response shows that the attitude control system is stable and effective.",
keywords = "Attitude control, LQR, Moving mass, Spinning spacecraft",
author = "Guo, {Peng Fei} and Zhao, {Liang Yu}",
year = "2013",
doi = "10.4028/www.scientific.net/AMR.760-762.1216",
language = "English",
isbn = "9783037857731",
series = "Advanced Materials Research",
pages = "1216--1220",
booktitle = "Optoelectronics Engineering and Information Technologies in Industry",
note = "2nd International Conference on Opto-Electronics Engineering and Materials Research, OEMR 2013 ; Conference date: 19-10-2013 Through 20-10-2013",
}