Adaptive Control for the Twin Rotor Helicopter with Actuator Faults

摘要：

　　For the linear time-invariant model of a twin-rotor helicopter,a new control scheme is proposed in the presence of actuator faults,environmental disturbances and modeling errors.Using the Lyapunov stability theorem,the system with proposed adaptive controller is proved to be stable,and the tracking error tends to zero asymptotically.Simulation results prove the effectiveness of this method.

关键词： Actuator Faults MRAC Twin Rotor Helicopter

作者: Shijun Zhang Fuyang Chen Gang Tao

作者单位: College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, China Department of Electrical and Computer Engineering, University of Virginia, USA

会议类型: 国际会议

会议名称: 3rd International Conference on Frontiers of Manufacturing and Design Science(第三届制造与设计科学前沿国际会议(ICFMD))

会议地点: 香港

会议语种:英文

页码: 1501-1505

在线出版日期: 2012-12-11（万方平台首次上网日期，不代表论文的发表时间）