Compensator Design for Helicopter Stabilization

被引：1

作者：

Goswami, Raghupati ^{[1
]}

Sanyal, Sourish ^{[2
]}

Sanyal, Amar Nath ^{[3
]}

机构：

[1] Ideal Inst Engn, Kalyani, W Bengal, India

[2] Coll Engn & Management, Kolaghat, W Bengal, India

[3] Jadavpur Univ Acad, Elect Engg, Aedconagar, W Bengal, India

来源：

2ND INTERNATIONAL CONFERENCE ON COMPUTER, COMMUNICATION, CONTROL AND INFORMATION TECHNOLOGY (C3IT-2012) | 2012年 / 4卷

关键词：

Helicopter; Feedback Control; Stabilization; Compensation;

D O I：

10.1016/j.protcy.2012.05.009

中图分类号：

TP18 [人工智能理论];

学科分类号：

081104 ; 0812 ; 0835 ; 1405 ;

摘要：

Helicopters are inherently unstable unlike aeroplanes. They are to be stabilized using appropriate feedback loops. A control structure with an inner and an outer loop is best-suited for them. The paper describes a design procedure for such a control scheme aiming at fulfilment of the design specs. The problem has been treated analytically with self-built programmes at first. Then recourse has been made to MATLAB control system window for refinement of the design. Finally SISOTOOL has been used to find out the best possible design configuration under given constraints. The design methodology yields a stable control system which has to be kept operative under flying conditions. (C) 2011 Published by Elsevier Ltd. Selection and/or peer-review under responsibility of C3IT

引用

页码：74 / 81

页数：8

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