Attitude Control of Missiles Via Finite-terms Fliess Ezpansion

摘要：

This paper investigates the attitude control of missiles. We use the decomposed Fliess functional expansion of input-output decomposable systems to describe the outputs. Then under piece-wise constant admissible value controls, the optimal control on.nite time durations can be obtained. The method tremendously reduces the complexity of computation and makes the online control design available. The effectiveness of the proposed method is shown by numerical simulations.

关键词： Nonlinear system Finite-terms Fliess functional ezpansion Input-output decoupling Attitude control

作者: Yupeng Qiao Dongbin Shen

作者单位: College of Automation Science and Engineering, South China University of Technology, Guangzhou 51064 College of Automation Science and Engineering,South China University of Technology, Guangzhou 510640

会议类型: 国际会议

会议名称: 2009年中国控制与决策会议(2009 Chinese Control and Decision Conference)

会议地点: 广西桂林

会议语种:英文

页码: 1021-1026

在线出版日期: 2009-06-17（万方平台首次上网日期，不代表论文的发表时间）