Global configuration stabilization for the VTOL aircraft with strong input coupling

被引：146

作者：

Olfati-Saber, R ^{[1
]}

机构：

[1] CALTECH, Dept Control & Dynam Syst, Pasadena, CA 91125 USA

来源：

IEEE TRANSACTIONS ON AUTOMATIC CONTROL | 2002年 / 47卷 / 11期

关键词：

autonomous vehicles; backstepping; differential flatness; global stabilization; nonlinear control;

D O I：

10.1109/TAC.2002.804457

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

Trajectory tracking and configuration stabilization for the vertical takeoff and landing (VTOL) aircraft has been so far considered in the literature only in the presence of a slight (or zero) input coupling (i.e., for a small epsilon). In this note, our main contribution is to address global configuration stabilization for the VTOL aircraft with a strong input coupling using a smooth static state feedback. In addition, the differentially flat outputs for the VTOL aircraft are automatically obtained as a by-product of applying a decoupling change of coordinates.

引用

页码：1949 / 1952

页数：4

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