Robust H2 Control with Adaptive Mechanism for the Yaw Control of Small-scale Helicopter

机译：自适应机制的鲁棒H2控制用于小型直升机的偏航控制

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This paper presents a robust H₂ controller design approach to the yaw control of a small-scale helicopter mounted on an experimental platform. The yaw dynamic system is linearized into a linear system, which is modelled by an affine uncertainty

机译：本文提出了一种鲁棒的H _{2 控制器设计方法，用于安装在实验平台上的小型直升机的偏航控制。偏航动态系统线性化为线性系统，并通过仿射不确定性建模}

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来源
《Robotics and Biomimetics, 2006 IEEE International Conference on; Kunming,China》||P.1197-1202|共6页
会议地点 KunmingChina
作者
Xingang Zhao; Zhe Jiang; Juntong Qi; Jianda Han; Guangjun Liu;
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原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Hsupinfin/sup control; adaptive control; aircraft control; control system synthesis; feedback; helicopters; linear matrix inequalities; linear systems; linearisation techniques; position control; robust control; uncertain systems; adaptive control; affine uncerta;

机译：H ^{infin 控制;自适应控制;飞机控制;控制系统综合;反馈;直升机;线性矩阵不等式;线性系统;线性化技术;位置控制;鲁棒控制;不确定系统;自适应控制;仿射无证;}

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4. Robust H2 Control with Adaptive Mechanism for the Yaw Control of Small-scale Helicopter [C] . Zhao, Xingang, Jiang, . 2006

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Robust H2 Control with Adaptive Mechanism for the Yaw Control of Small-scale Helicopter

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