Nonlinear Internal Model Based Attitude Tracking and Disturbance Rejection of Rigid Spacecraft

摘要：

In this paper, we consider the attitude tracking and disturbance rejection problem of rigid spacecraft subject to a class of nonharmonic periodic disturbances generated by nonlinear exosystems, which can not be handled by linear internal model. A nonlinear internal model is designed to deal with such disturbances. Numerical simulations illustrate the performance of the proposed control algorithms.

作者: Xuxi Zhang Xianping Liu

作者单位: College of Science Harbin Engineering University Harbin, China, 150001 College of Science Harbin Engineering University Harbin, China,l50001

会议类型: 国际会议

会议名称: 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems(2010 IEEE 智能计算与智能系统国际会议 ICIS 2010)

会议地点: 厦门

会议语种:英文

页码: 711-715

在线出版日期: 2010-10-29（万方平台首次上网日期，不代表论文的发表时间）