Design of Gain Scheduled H∞ Flight Control Law Satisfying Specified Stability Margin

Yasuhiro Yamaguchi; Masahiro Ohno; Takashi Hata

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Design of Gain Scheduled H∞ Flight Control Law Satisfying Specified Stability Margin

机译：满足规定稳定裕度的计划增益H∞飞行控制律设计

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This paper proposes gain scheduled H∞ flight control design method, which can satisfy specified stability margin. The parameter changes due to flight conditions are described by LPV (Linear Parameter Varying) model, and gain scheduled controller is designed by LMI (Linear Matrix Inequality) theory. Stability margin requirements can be described as a kind of mixed sensitivity H∞ problem with constant weighting.

机译：提出了一种满足预定稳定裕度的增益调度H∞飞行控制设计方法。由飞行条件引起的参数变化由LPV（线性参数变化）模型描述，增益调度控制器由LMI（线性矩阵不等式）理论设计。稳定性裕量要求可以描述为一种具有恒定权重的混合灵敏度H∞问题。

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来源
《日本航空宇宙学会論文集》 |2000年第561期|p.322-328|共7页
作者
Yasuhiro Yamaguchi; Masahiro Ohno; Takashi Hata;
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原文格式 PDF
正文语种 jpn
中图分类航空;
关键词
flight control; gain Scheduling; stability margin;

机译：飞行控制;获得调度;稳定裕度;

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1. Design of Gain Scheduled H∞ Flight Control Law Satisfying Specified Stability Margin [J] . Yasuhiro Yamaguchi, Masahiro Ohno, Takashi Hata 日本航空宇宙学会論文集 . 2000,第561期

机译：满足规定稳定裕度的计划增益H∞飞行控制律设计
2. Design of a gain-scheduling mechanism for flight control laws by fuzzy clustering [J] . M. Oosterom, R. Babuska Control Engineering Practice . 2006,第7期

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Design of Gain Scheduled H∞ Flight Control Law Satisfying Specified Stability Margin

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