Robust control law design for a small commercial aircraft

被引：0

作者：

Amato, F ^{[1
]}

Iervolino, R ^{[1
]}

Ciniglio, U ^{[1
]}

Verde, L ^{[1
]}

机构：

[1] Univ Naples Federico II, Dipartimento Informat & Sistemist, I-80125 Naples, Italy

来源：

AUTOMATIC CONTROL IN AEROSPACE 2001 | 2002年

关键词：

Robust MIMO flight control design; mu theory; small commercial aircraft;

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 modem multi-input multi-output (MIMO) control design techniques could significantly contribute to the reduction of the development time and cost of a fly-by-wire flight control system also for a small commercial aircraft. Moreover, they allow taking into account system robustness properties for stability and performance with respect to the unavoidable model uncertainties. In this paper the potential benefits of the mu analysis and synthesis theory to the flight control law design are evaluated by means of a practical benchmark problem. Copyright mu 2001 IFAC.

引用

页码：279 / 284

页数：6

共 11 条

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