Modeling and Attitude Control of a Spinning Spacecraft with Internal Moving Mass

摘要：

　　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.

关键词： spinning spacecraft moving mass LQR attitude control

作者: Pengfei Guo Liangyu Zhao

作者单位: School of Aerospace Engineering Beijing Institute of Technology Beijing 100081,China

会议类型: 国际会议

会议名称: 2013 2nd International Conference on Computer Science and Electronics Engineering(ICCSEE2013)(2013年第二届计算机科学与电子工程国际会议)

会议地点: 杭州

会议语种:英文

页码: 2939-2942

在线出版日期: 2013-03-22（万方平台首次上网日期，不代表论文的发表时间）