Missile Guidance Law Design using Nonlinear Robust Output Regulation and T-S Model
This paper is concerned with the design of missile guidance law based on robust output regulation theory and Takagi – Sugeno fuzzy model. In this design, the guidance problem is converted to the nonlinear regulator problem. The three-dimensional (3-D) command to line-of-sight (CLOS) guidance problem is formulated as a tracking problem of a time-varying nonlinear system. It is provided the solution in terms LMIs allowing the use of numeric techniques in the search of a guidance controller. Simulation results for different engagement scenarios illustrate the validity of the proposed guidance law.
Li-Ying YUAN Shi-Yong LI
Harbin Institute of Technology, China
国际会议
2nd IEEE Conference on Industrial Electronics and Applications(ICIEA 2007)(第二届IEEE工业电子与应用国际会议)
哈尔滨
英文
2007-05-23(万方平台首次上网日期,不代表论文的发表时间)