Adaptive Fault-tolerant Controller Design for a Class of Hypersonic Aircraft with Actuator Failure

摘要：

To solve the part of actuator failure problem,the nonlinear observer and controller are designed synthetically.We develop the research model based on a SISO output feedback nonlinear unobservered minimum phase system under the condition of single channel actuator failure of the hypersonic aircraft,adopt filter to reconstruct state vectors,design the adaptive control law to guarantee the system boundedness.The pitch channel of hypersonic aircraft is studied as an example to validate above theory.

作者: CHEN Jie PAN Changpeng ZHAO Hongchao

作者单位: Department of Control Engineering ,Naval Aeronautical and Astronautical University,Yantai,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）