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综合飞行/矢量推进系统控制器分离方法
引用本文:李彦双,孙健国. 综合飞行/矢量推进系统控制器分离方法[J]. 中国现代应用药学, 2009, 24(12)
作者姓名:李彦双  孙健国
作者单位:南京航空航天大学,南京航空航天大学
摘    要:详细阐述了综合飞行/矢量推进系统控制器分离问题,并给出了采用解析法求解控制器分离问题的步骤。以解析的控制器分离为基础,提出了一种基于非线性最小二乘方法的控制器分离的优化方案,本文中所给的优化方案非常有效并且很便于实现。利用此优化方案,求取了一个最优的控制器分离。非线性仿真实验表明,最优分离子控制器几乎达到了同集中控制器一样的闭环性能,这意味着本文所讨论的控制器分离方案是相当合适和成功的。

关 键 词:综合飞行/矢量推进系统;控制器分离;优化;非线性最小二乘;非线性仿真
修稿时间:2009-03-27

Controller Partitioning for Integrated Flight/Vectoring Propulsion Control
Li Yan-shuang and Sun Jian-guo. Controller Partitioning for Integrated Flight/Vectoring Propulsion Control[J]. The Chinese Journal of Modern Applied Pharmacy, 2009, 24(12)
Authors:Li Yan-shuang and Sun Jian-guo
Affiliation:Nanjing University of Aeronautics and Astronautics,Nanjing University of Aeronautics and Astronautics
Abstract:The controller partitioning problem for the integrated flight/vectoring propulsion control is presented in detail and an analytical controller partitioning is obtained using a stepwise procedure. Based on the results of the analytical controller partitioning, an optimization scheme for controller partitioning using nonlinear least-squares method is proposed. The optimization scheme proposed in this paper is quite effective and easy to realize. Then an optimal controller partitioning is obtained using the optimization scheme for the integrated flight/vectoring propulsion control. The experiments on many nonlinear simulation examples demonstrate that the performance of closed-loop system with the optimal partitioned subcontrollers is almost the same as that achieved by the centralized controller, which means that the controller partitioning scheme discussed in this paper is quite suitable and successful.
Keywords:integrated flight/vectoring propulsion control   controller partitioning   optimization   nonlinear least-squares   nonlinear simula-tion
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