Optimal H-infinity design of a glide-slope coupler

被引：0

作者：

Dragan, V ^{[1
]}

Stoica, A ^{[1
]}

机构：

[1] Inst Math Romanian Acad, RO-70700 Bucharest, Romania

来源：

SYSTEM STRUCTURE AND CONTROL 1997 | 1998年

关键词：

H-infinity control; numerical algorithms; aerospace control; singular perturbation method; optimal control;

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 aim of the paper is to present a method for the design of a glide-slope coupler of an aircraft using an optimal H-infinity approach obtained via the theory of singularly perturbed systems. The benefits of this optimal design procedure are emphasized by comparing computational aspects, tracking and robustness performances with the ones obtained when using suboptimal H-infinity methods. Copyright (C) 1998 IFAC.

引用

页码：249 / 253

页数：5

共 11 条

[1]

Breslin S. G., 1995, Proceedings of the Third European Control Conference. ECC 95, P3134

[2] STATE-SPACE SOLUTIONS TO STANDARD H-2 AND H-INFINITY CONTROL-PROBLEMS [J].