Robust Hurwitz Stability and Performance Analysis of H-Infinity Controlled Forward-Velocity Dynamics of UAVs in Close Formation Flight Using Bounded Phase Conditions in a Kharitonov Framework

被引：9

作者：

Johnson Y. ^{[1
]}

Dasgupta S. ^{[2
]}

机构：

[1] EEE Department, CET, Trivandrum

[2] EEE Department, MCET, Trivandrum, Kerala

来源：

Journal of The Institution of Engineers (India): Series C | 2014年 / 95卷 / 03期

关键词：

Bounded phase; Kharitonov polynomials; Robust H-infinity; UAV formation flight;

D O I：

10.1007/s40032-014-0136-y

中图分类号：

学科分类号：

摘要：

Multiple unmanned aerial vehicle (UAV) control in formation flight is comparatively a new research area in the field of aerospace engineering. In the proposed work, robust control techniques are implemented to maintain a fixed relative distance in horizontal and vertical direction with uniform pitch orientation in an uncertain leader–follower pattern of close formation flight platform. The forward velocity dynamics is of focal interest in this paper. H-infinity controllers are designed for leader control and its tracking. The robustness of the H-infinity controller is validated with Kharitonov related bounded phase conditions by forming interval polynomials. © 2014, The Institution of Engineers (India).

引用

页码：223 / 231

页数：8

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