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Adaptive block dynamic surface control for integrated missile guidance and autopilot
  • ISSN号：1000-9361
  • 期刊名称：Chinese Journal of Aeronautics
  • 时间：2013.6
  • 页码：741-750
  • 分类：TP13[自动化与计算机技术—控制科学与工程;自动化与计算机技术—控制理论与控制工程] TN31[电子电信—物理电子学]
  • 作者机构：[1]Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China
  • 相关基金：This wore was supported by National Basic Research Program of China （973 Program） （No. 2012CB821205）, National Natural Science Foundation of China （Nos. 61021002 and 61203125）, and Fundamen- tal Research Funds for the Central Universities （No. HIT. NSRIF. 2013039）.
  • 相关项目：具有输入饱和非线性的导引与控制一体化全耦合设计方法研究
作者： Hou Mingzhe|Liang Xiaoling|Duan Guangren|
关键词： 随机非线性系统, 输出反馈镇定, 开关切换, Lyapunov函数, 任意性, 输出反馈控制器, 噪声驱动, 反馈形式, Stochastic nonlinear system, switched nonlinear system, output feedback, under arbitrary switchings, moment expo-nential stability.
中文摘要：

这份报纸在任意的切换下面为交换随机的非线性的系统的一个类在概率涉及全球输出反馈稳定的问题。分系统被假定在产量反馈形式并且由白噪音开车。由介绍普通 Lyapunov 功能，交换信号的普通产量反馈控制器独立人士基于 backstepping 途径被构造。靠近环的系统的零个解决方案指数地是第四时刻的，这被证明稳定。一个例子被给显示出建议方法的有效性。

英文摘要：

This paper is concerned with the problem of global output feedback stabilization in probability for a class of switched stochastic nonlinear systems under arbitrary switchings. The subsystems are assumed to be in output feedback form and driven by white noise. By introducing a common Lyapunov function, the common output feedback controller independent of switching signals is constructed based on the backstepping approach. It is proved that the zero solution of the closed-loop system is fourth-moment exponentially stable. An example is given to show the effectiveness of the proposed method.

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期刊信息
  • 《中国航空学报：英文版》
  • 中国科技核心期刊
  • 主管单位:中国航空工业第一集团公司
  • 主办单位:中国航空学会
  • 主编：朱自强
  • 地址：北京学院路37号中国航空学报：英文版编辑部
  • 邮编：100083
  • 邮箱：caifei@buaa.edu.cn
  • 电话：010-82317058 82318016
  • 国际标准刊号：ISSN：1000-9361
  • 国内统一刊号：ISSN：11-1732/V
  • 邮发代号:
  • 获奖情况:
  • 国内外数据库收录:
  • 被引量:393