Robust decoupling control design for twin rotor system using Hadamard weights

Q. Ahmed, A. I. Bhatti, S. Iqbal
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引用次数: 24

Abstract

This paper considers cross-coupling affects in a twin rotor system that leads to degraded performance during precise helicopter maneuvering. This cross-coupling can be suppressed implicitly either by declaring it as disturbance or explicitly by introducing decoupling techniques. The standard H∞ controller synthesized by loop-shaping design procedure (LSDP) offers robustness at the cost of performance to overcome cross-coupling. However, Hadamard weights are used to decouple the system dynamics to give desired performance as well. This idea has been successfully proved by simulations and verified through implementing it on a twin rotor system.
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基于Hadamard权值的双转子系统鲁棒解耦控制设计
本文研究了双旋翼系统中交叉耦合效应导致的直升机精密机动性能下降问题。这种交叉耦合可以通过将其声明为干扰来隐式抑制,也可以通过引入解耦技术来显式抑制。由环形设计程序(LSDP)合成的标准H∞控制器以性能为代价提供鲁棒性以克服交叉耦合。然而,使用Hadamard权值来解耦系统动力学以获得期望的性能。通过仿真验证了该方法的有效性,并在某双转子系统上进行了验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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