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Method of fitting the solution of SDRE with polynomial
Wu, Li-Ye ; Yu, Zhen ; Liu, Li-Jun ; Yu Z(余臻) ; Liu LJ(刘利军)
2014
关键词Controllers Electronic guidance systems Equations of state Guided missiles Riccati equations
英文摘要Conference Name:Proceedings of the 33rd Chinese Control Conference, CCC 2014. Conference Address: Nanjing, China. Time:July 28, 2014 - July 30, 2014.; Systems Engineering Society of China; Technical Committee on Control Theory of Chinese Association of Automation; The State-dependent Riccati equation (SDRE) method is widely used in the suboptimal controller design, but the SDRE is difficult to solve. In this paper, a new method that based on polynomial fitting is proposed for the solution of SDRE. And it is used in the design of missile guidance law for impact angel constrained to zero. Compared to the existing methods, it has obvious advantages in accuracy and calculation on line. What is more, the final solution has analytical form, which has good properties for the analysis and improvement. Simulation results are also given to demonstrate that it is accurate and clear, which can replace the real solution of SDRE. ? 2014 TCCT, CAA.
语种英语
出处http://dx.doi.org/10.1109/ChiCC.2014.6896956
出版者IEEE Computer Society
内容类型其他
源URL[http://dspace.xmu.edu.cn/handle/2288/86945]  
专题信息技术-会议论文
推荐引用方式
GB/T 7714
Wu, Li-Ye,Yu, Zhen,Liu, Li-Jun,et al. Method of fitting the solution of SDRE with polynomial. 2014-01-01.
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