Exact steering and stabilization of a PVTOL aircraft

被引：0

作者：

Di Giamberardino, P ^{[1
]}

Djemai, M ^{[1
]}

Monaco, S ^{[1
]}

Normand-Cyrot, D ^{[1
]}

机构：

[1] Univ Rome La Sapienza, Dipartimento Informat & Sistemist, I-00184 Rome, Italy

来源：

PROCEEDINGS OF THE 36TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-5 | 1997年

关键词：

epsilon non minimum phase; steering; multirate digital control; exact sampling;

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：

In this paper a piecewise continuous control law for maneuvering a PVTOL aircraft is proposed. The control scheme is composed by two loops: a continuous inner state feedback together with an outer piecewise constant one. The design procedure, based on some recent results on exact sampling and multirate techniques is briefly introduced and applied to our case study. An additional digital feedback is used to improve the robustness of the control scheme. Some simulation results are reported in order to show the effectiveness of the proposed control strategy.

引用

页码：2049 / 2054

页数：6