Directional change in multivariable LQG control with actuator failure

Horla D.

首页> 外文期刊>Bulletin of the Polish Academy of Sciences. Technical Sciences >Directional change in multivariable LQG control with actuator failure

【24h】

Directional change in multivariable LQG control with actuator failure

机译：具有执行器故障的多变量LQG控制的定向变化

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

The paper presents the phenomenon of directional change in LQG control of multivariable systems with amplitude constraints, as well as the impact of the latter on control performance. The interplay of directional change of the computed control vector with control performance has been thoroughly investigated, and is a result of the presence of constraints imposed on the applied control vector for different proportions of the number of control inputs to plant outputs. The impact of directional change phenomenon on the control performance has been defined, stating that performance deterioration is not tightly coupled with preservation of direction of the computed control vector. The statement has been supported by numerous simulation results for different types of plants with different LQG controller parameters.

机译：本文研究了具有振幅约束的多变量系统LQG控制中的方向变化现象，以及后者对控制性能的影响。计算出的控制矢量的方向变化与控制性能之间的相互作用已被彻底研究，这是由于控制输入与电厂输出的不同比例对应用的控制矢量施加了约束的结果。定义了方向变化现象对控制性能的影响，指出性能恶化与保持计算控制向量的方向不是紧密耦合的。这一说法得到了不同LQG控制器参数的不同类型对象的大量仿真结果的支持。

著录项

来源
《Bulletin of the Polish Academy of Sciences. Technical Sciences》 |2017年第4期|共10页
作者
Horla D.;
展开▼
作者单位

Poznan Univ Tech Fac Elect Engn 3A Piotrowo St PL-60965 Poznan Poland;

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类一般工业技术;年鉴、年刊;
关键词
directional change; actuator failure; windup phenomenon;

机译：定向变化;执行器故障;卷绕现象;

相似文献

外文文献
中文文献
专利

1. Reconfigurable fault-tolerant control for supersonic missiles with actuator failures under actuationredundancy [J] . Tong LI, Zhenyu JIANG, Huabo YANG, 中国航空学报（英文版） . 2020,第001期
2. Time-varying fault-tolerant formation tracking based cooperative control and guidance for multiple cruise missile systems under actuator failures and directed topologies [J] . XU Xingguang, WEI Zhenyan, REN Zhang, 系统工程与电子技术（英文版） . 2019,第003期
3. Robust fault-tolerant control for wing flutter under actuator failure [J] . Gao Mingzhou, Cai Guoping 中国航空学报（英文版） . 2016,第004期
4. A parameter estimation based adaptive actuator failure compensation control scheme [J] . Gang Tao, Ruiyun Qi, Chang Tan 系统工程与电子技术：英文版 . 2011,第001期
5. Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures [J] . HU Qinglei, ZHANG Youmin, HUO Xing, 中国航空学报：英文版 . 2011,第001期
6. Directional change in multivariable LQG control with actuator failure [J] . D. HorlaCorresponding authorFaculty of Electrical Engineering Poznan University of Technology 3A Piotrowo St. 60-965 Poznan PolandEmailOther articles by this author:De Gruyter OnlineGoogle Scholar Bulletin of the Polish Academy of Sciences. Technical Sciences . 2017,第4期

机译：执行器故障时多变量LQG控制的方向变化
7. Directional change in multivariable LQG control with actuator failure [J] . Horla D. Bulletin of the Polish Academy of Sciences. Technical Sciences . 2017,第4期

机译：具有执行器故障的多变量LQG控制方向变化
8. Directional change and windup phenomena in LQR-controlled systems with actuator failure [J] . Dariusz Horla Archives of Electrical Engineering . 2018,第2期

机译：具有执行器故障的LQR控制系统中的定向变化和卷绕现象
9. DIRECTIONAL CHANGE ISSUES IN LQG CONTROL WITH ACTUATOR FAILURE [C] . Dariusz Horla IFAC Conference on Manufacturing Modelling, Management, and Control . 2013

机译：LQG控制与执行器故障的定向变更问题
10. Synthesis of actuator limited multivariable control systems. [D] . Mulder, Eric Franklin. 2003

机译：执行器受限的多变量控制系统的综合。
11. Decentralized Sliding Mode Observer Based Dual Closed-Loop Fault Tolerant Control for Reconfigurable Manipulator against Actuator Failure [O] . Bo Zhao, Chenghao Li, Derong Liu, -1

机译：基于分散滑模观测器的双闭环容错控制用于可重构机械手以防止执行器故障
12. MULTIVARIABLE LQG VIBRATION CONTROL USING CHARGE-DRIVEN PIEZOELECTRIC ACTUATORS [O] . 2015

机译：采用电荷驱动的压电驱动器的多变量LQG振动控制
13. Multivariable Control of a Twin Lift Helicopter System Using the LQG/LTR Design Methodology [R] . Rodriguez, A. A., Athans, M. 1986

机译：基于LQG / LTR设计方法的双升力直升机系统的多变量控制

Directional change in multivariable LQG control with actuator failure

摘要

著录项

相似文献

相关主题

期刊订阅