Fault Tolerant Flight Control Law Design with a Model-Following Sliding Mode Controller
A sfiding mode controller based on model following control is designed for the fright control system with uncertainties and perturbations. With this controller, the controlled plant can track the reference model precisely. It is shown that this scheme provides better performance for the flight control system and the fault tolerant control objective is achieved. The proposed scheme has the advantages of the model following and sllding-mode control. A Proportional Integral type sfiding surface is designed through pole placement method to make the sliding mode have good dynamic characteristics and to eliminate the steady state error. The simple saturation control is adopted to weaken the chattering phenomena. The simulation results show that the flight control system using this controUer not only doesnt require the procedure of fault detection and isolation, but also achieves the model following.
fault tolerant flight control sliding mode control model following control
Yang Zhi-jun Qi Xiao-hui Shan Gan-lin
Department of Optical and Electronic Engineering Mechanical Engineering College Shijiazhuang 050003,China
国际会议
长沙
英文
665-668
2009-04-11（万方平台首次上网日期，不代表论文的发表时间）