Nonlinear Observer and Controller Design for a Class of Hypersonic Aircraft with Sensor Failure

摘要：

To solve the sensor failure problem,the nonlinear observer and controller are designed respectively.Under the condition of output measureable only,the paper designs a novel extended Luenberger form observer to estimate convergence state vector and brings forward a new strong adaptive control law based on dynamic surface adaptive backstepping control. Finally,the results are verified by simulation for a 6 DOF hypersonic aircraft.

作者: CHEN Jie PAN Changpeng WU Jinhua

作者单位: Naval Aeronautical and Astronautical University,Yantai 264001,Shandong,P.R.China

会议类型: 国际会议

会议名称: The 30th Chinese Control Conference(第三十届中国控制会议)

会议地点: 烟台

会议语种:英文

页码: 1-6

在线出版日期: 2011-07-01（万方平台首次上网日期，不代表论文的发表时间）