Gain Scheduling Control of Nonlinear Shock Motion Based on Equilibrium Manifold Linearization Model
The equilibrium manifold linearization model of nonlinear shock motion is of higher accuracy and lower complexity over other models such as the small perturbation model and the piecewise-linear model. This paper analyzes the physical significance of the equilibrium manifold linearization model, and the self-feedback mechanism of shock motion is revealed. This helps to describe the stability and dynamics of shock motion. Based on the model, the paper puts forwards a gain scheduling control method for nonlinear shock motion. Simulation has shown the validity of the control scheme.
作 者： Cui Tao Yu Daren Bao Wen Yang Yongbin 作者单位： College of Energy Science and Engineering, Harbin Institute of Technology, Harbin 150001, China 刊 名： 中国航空学报(英文版) ISTIC 英文刊名： CHINESE JOURNAL OF AERONAUTICS 年，卷(期)： 2007 20(6) 分类号： V2 关键词： shock motion equilibrium manifold linearization gain scheduling control