Control allocation for a V/STOL aircraft based on robust fuzzy control

被引：8

作者：

Fan Yong ^{[1
]}

Meng XianYu ^{[1
]}

Yang XiLi ^{[1
]}

Liu Kai ^{[1
]}

Zhu JiHong ^{[1
]}

机构：

[1] Tsinghua Univ, Dept Sci & Technol, Beijing 100084, Peoples R China

来源：

SCIENCE CHINA-INFORMATION SCIENCES | 2011年 / 54卷 / 06期

基金：

中国国家自然科学基金;

关键词：

V/STOL; tailless; robust control; fuzzy; control allocation; H-INFINITY-CONTROL; NONLINEAR-SYSTEMS;

D O I：

10.1007/s11432-011-4257-0

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

This study addresses the design of an output-feedback H-infinity and fuzzy mixed controller for an advanced vertical and/or short take-off and landing aircraft that exhibits satisfactory global stability criteria. A fuzzy logic based optimization approach is employed to solve autonomously the constrained control allocation problem by suitably adjusting the components of the output vector and finding a proper vector in the attainable moment set. Simulations show that the designed fuzzy controller is better suited to resist external disturbances, and is robust against parameter perturbations.

引用

页码：1321 / 1326

页数：6

共 50 条

[1] Control allocation for a V/STOL aircraft based on robust fuzzy control
FAN Yong
ScienceChina(InformationSciences), 2011, 54 (06) : 1321 - 1326
[2] Control allocation for a V/STOL aircraft based on robust fuzzy control
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XianYu Meng
XiLi Yang
Kai Liu
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Science China Information Sciences, 2011, 54 : 1321 - 1326
[3] CONTROL OF V/STOL AIRCRAFT
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[5] CONTROL OF V/STOL AIRCRAFT.
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[6] PROPULSION CONTROL CONSIDERATIONS FOR V/STOL AIRCRAFT
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[7] REACTION CONTROL SYSTEMS FOR V/STOL AIRCRAFT
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