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.
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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