A gain scheduling approach for a flexible aircraft

被引：0

作者：

Aouf, N ^{[1
]}

Boulet, B ^{[1
]}

Botez, R ^{[1
]}

机构：

[1] McGill Univ, Ctr Intelligent Machines, Montreal, PQ H3A 2A7, Canada

来源：

PROCEEDINGS OF THE 2002 AMERICAN CONTROL CONFERENCE, VOLS 1-6 | 2002年 / 1-6卷

关键词：

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：

A technique based on interpolation of the solutions of Riccati equations for frozen H-infinity designs is used for gain scheduling over the full flight envelope of a flexible aircraft. The aircraft model consists of a linear parameter-varying model of a flexible B1 bomber that varies with the Mach number from 0.2 to 0.8Mach. The performance objectives are to track the pitch demand and to alleviate the loads due to wind gusts. The flexibility of the aircraft is taken into account through four flexible modes. The method presented is shown to provide good results over the full flight envelope, while allowing for a simple implementation structure.

引用

页码：4439 / 4442

页数：4

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