Modeling and Attitude Control of a Spinning Spacecraft with Internal Moving Mass
Pengfei Guo, Liangyu Zhao
Available Online March 2013.
- https://doi.org/10.2991/iccsee.2013.733How to use a DOI?
- spinning spacecraft, moving mass, LQR, attitude control
- 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 linear-quadratic-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.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Pengfei Guo AU - Liangyu Zhao PY - 2013/03 DA - 2013/03 TI - Modeling and Attitude Control of a Spinning Spacecraft with Internal Moving Mass BT - Proceedings of the 2nd International Conference on Computer Science and Electronics Engineering (ICCSEE 2013) PB - Atlantis Press SP - 3172 EP - 3175 SN - 1951-6851 UR - https://doi.org/10.2991/iccsee.2013.733 DO - https://doi.org/10.2991/iccsee.2013.733 ID - Guo2013/03 ER -