Output Feedback Stabilization Design of PVTOL Aircraft Based on a Finite-time Observer

被引：0

作者：

Zhang, Juan ^{[1
]}

Li, Meng ^{[1
]}

机构：

[1] Cent S Univ, Sch Informat Sci & Engn, Changsha 410083, Hunan, Peoples R China

来源：

2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC) | 2017年

基金：

中国国家自然科学基金;

关键词：

PVTOL aircraft; finite-time observer; output feedback; saturation technique; VTOL AIRCRAFT; SYSTEMS; SATURATION; TRACKING;

D O I：

暂无

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 note considers output feedback stabilization design of PVTOL aircraft without velocity measurements. When the model states are recovered by the observer, a saturation technique is used to construct the controller. Without using backstepping, the controller is simple and the global convergence analysis is straightforward. The effectiveness of the algorithm is illustrated by simulation results.

引用

页码：2865 / 2869

页数：5

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