Partial linearization of the PVTOL aircraft with internal stability

被引：0
|
作者：
Lechappe, V. [1 ]
Aoustin, Y. [1 ]
Marquez-Martinez, L. A. [2 ]
Moog, C. H. [1 ]
机构：
[1] Univ Nantes, Ecole Cent Nantes, UMR CNRS 6597, LUNAM IRCCyN, F-44035 Nantes, France
[2] CICESE Res Ctr Ensenada BC Mexico, Ensenada, Baja California, Mexico
来源：
2013 IEEE 52ND ANNUAL CONFERENCE ON DECISION AND CONTROL (CDC) | 2013年
关键词：
nonlinear; MIMO; underactuated; non-minimum phase; zero-dynamics; internal dynamics; algebraic method; partial linearization; stabilization; PVTOL; NONLINEAR CONTROL DESIGN; STABILIZATION;
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：
The planar vertical take-off and landing (PVTOL) aircraft is worked out by inspecting the various feedback linearization solutions. Partial linearizations of the state space are performed, which ensure the stability of the associated internal dynamics. The results are obtained through the search of dummy outputs with a 0-dimensional, 1-dimensional or 2-dimensional zero-dynamics that are stable.
引用
收藏
页码：2564 / 2569
页数：6
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