One Near Space Hypersonic Aircraft Attack Angle Observer and Controller Design

摘要：

A novel sliding surface observer and controller is designed based on Lyapunov function for hypersonic aircraft nonlinear dynamitic system. Overload output sliding surface to construct Lyapunov function to guarantee the astringency of observer. Dynamic surface adaptive backstepping is adopted designed to ensure control law, and multi-layers neural network adjust function is used to compensate the influence from the uncertain, which designs the robust terms to solve the problem from approach error. The stability analysis and simulations demonstrate the good performance of the controller.

关键词： Dynamic surface adaptive backstepping Observer Uncertain Hypersonic aircraft Multi-layers neural network

作者: CHEN Jie PAN Changpeng ZHAO Hongchao

作者单位: Naval Aeronautical and Astronautical University, Yantai, Shandong Province, China Naval Aeronautical and Astronautical University, China

会议类型: 国际会议

会议名称: 2011 China Control and Decision Conference(2011中国控制与决策会议 CCDC)

会议地点: 四川绵阳

会议语种:英文

页码: 2724-2729

在线出版日期: 2011-05-23（万方平台首次上网日期，不代表论文的发表时间）