Robust Control of 2-DoF Helicopter System in Presence of Unmatched Disturbances & Actuator Faults

Keyur Rathod, Mija S.J.
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引用次数: 1

Abstract

This paper focuses on the design of robust controllers for the stabilization of CE 150 Humusoft 2-DoF Helicopter system which represents a highly nonlinear & cross coupled system usually subject to external disturbances and parametric uncertainties. A two loop control architecture is used where the inner loop ensures stabilization, error minimization and robustness to parametric uncertainties, matched & unmatched disturbances and the outer loop ensures optimal trajectory tracking without violating actuator saturation bounds. Further, to show the performance of the proposed control scheme, simulation results are presented.
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存在非匹配扰动和执行器故障的二自由度直升机系统鲁棒控制
ce150直升机系统是一个高度非线性交叉耦合系统,经常受到外界干扰和参数不确定性的影响,本文研究了该系统的鲁棒控制器设计。采用两环控制体系结构,其中内环确保稳定,误差最小化和对参数不确定性,匹配和不匹配干扰的鲁棒性,外环确保在不违反执行器饱和边界的情况下进行最佳轨迹跟踪。为了验证所提控制方案的有效性,给出了仿真结果。
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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