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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].航空动力学报,2009,24(12):2714-2820.
作者姓名:李彦双  孙健国
作者单位:南京航空航天大学能源与动力学院,南京,210016
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,该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,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
收稿时间:2008/11/28 0:00:00
修稿时间:3/27/2009 4:34:34 PM

Controller partitioning method for integrated flight/vectoring propulsion control
LI Yan-shuang and SUN Jian-guo.Controller partitioning method for integrated flight/vectoring propulsion control[J].Journal of Aerospace Power,2009,24(12):2714-2820.
Authors:LI Yan-shuang and SUN Jian-guo
Institution: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 simulation
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