Observer-based nonlinear stabilization control design for flexible satellite attitude system

摘要：

　　In this paper,an observer-based nonlinear stabilization control method is presented for the problem of flexible satellite attitude maneuver and vibration suppression.By introducing the auxiliary variables,the attitude mode of flexible satellite is converted into the corresponding nonlinear polynomial state space description.According to the structural features of attitude system,the nonlinear state feedback controller based on the reduced-order observer is obtained by using the Lyapunov theory and polynomial sum of squares (SOS) method.Finally,the proposed approach is applied to the attitude control of a flexible satellite and the simulation results show that both the fast rotational maneuver and the vibration suppression are well realized.

关键词： Nonlinear stabilization control Reduced-order observer Sum of squares Flexible satellite Attitude maneuver

作者: ZHOU Yanru CAI Xihai ZENG Jianping

作者单位: School of Information Science and Technology,Xiamen University,Xiamen Fujian 361005

会议类型: 国际会议

会议名称: The 33th Chinese Control Conference第33届中国控制会议

会议地点: 南京

会议语种:英文

页码: 1806-1810

在线出版日期: 2014-07-28（万方平台首次上网日期，不代表论文的发表时间）