Reliable computation of the robustness margin for a flexible aircraft

被引：18

作者：

Ferreres, G ^{[1
]}

Biannic, JM ^{[1
]}

机构：

[1] Off Natl Etud & Rech Aerosp, CERT, DCSD, F-31055 Toulouse 4, France

来源：

CONTROL ENGINEERING PRACTICE | 2001年 / 9卷 / 12期

关键词：

robustness analysis; structured singular value; flexible aircraft;

D O I：

10.1016/S0967-0661(01)00039-9

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, an efficient method for directly computing a reliable estimate of the maximal structured singular value mu is proposed, A method, which directly computes a mu upper bound over a frequency interval, is first extracted from Ferreres and Biannic (Proc. ACC 4 (1998) 2294-2298). The problem is then to evaluate the conservatism of this upper bound by computing an accurate P lower bound which is the central issue of the paper. The proposed algorithm is successfully applied-with a reasonable computational effort-to a challenging aeronautical application, namely the evaluation of the robustness properties of the flight control system of a flexible transport aircraft. (C) 2001 Elsevier Science Ltd. All rights reserved.

引用

页码：1267 / 1278

页数：12

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