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Nonlinear Control for a Model-scaled Helicopter with Constraints on Rotor Thrust and Fuselage Attitude

ZHU Bing HUO Wei

自动化学报Issue(11)：2654-2664,11.

自动化学报Issue(11)：2654-2664,11.DOI:10.3724/SP.J.1004.2014.02654

Nonlinear Control for a Model-scaled Helicopter with Constraints on Rotor Thrust and Fuselage Attitude

ZHU Bing ¹HUO Wei¹

作者信息

1. The Seventh Research Division, Beihang University, Beijing 100191, China
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摘要

关键词

Nonlinear control/trajectory tracking/helicopter control/saturated control

Key words

Nonlinear control/trajectory tracking/helicopter control/saturated control

引用本文复制引用

ZHU Bing,HUO Wei..Nonlinear Control for a Model-scaled Helicopter with Constraints on Rotor Thrust and Fuselage Attitude[J].自动化学报,2014,(11):2654-2664,11.

基金项目

Supported by National Natural Science Foundation of China (61074010) （61074010）

自动化学报

OA北大核心CSCDCSTPCD

ISSN：0254-4156

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