Sliding mode control for an aerodynamic missile based on backstepping design
Wenjin GU
Hongchao ZHAO
Changpeng PAN
摘要：In order to solve the mismatched uncertainties of a class of nonlinear systems,a control method of sliding mode control (SMC) based on the backstepping design is proposed.It introduces SMC in to the last step of backstepping design to modify the backstepping algorithm.This combination not only enables the generalization of the backstepping design to be applied to more general nonlinear systems,but also makes the SMC method become effective in solving the mismatched uncertainties.The SMC based on the backstepping design is applied to the flight control system design of an aerodynamic missile.The control system is researched through simulation.The simulation results show the effectiveness of the proposed control method.
机标关键词：backstepping designmismatched uncertaintiesgeneral nonlinear systemscontrol system designcontrol methodbackstepping algorithmsliding mode controlaerodynamic missile
分类号：TJ7(火箭、导弹)
论文发表日期：2005-01-01
在线出版日期：2025-08-15（本平台首次上网日期，不代表文献的发表时间）
页数：5( 71-75 )
英文信息