Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme

The control scheme of a robotic coax-helicopter was investigated and a control scheme was proposed to simultaneously satisfy not only nominal performance and robust performance but also the complexity, flexibility, and computation of controller design. The complete dynamics was considered including...

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Main Authors: Yan-li Chen, Jing-chun Qin, Zhi-yan Dong, Shun-an Liu, Heng-liang Zheng
Format: Article
Language:English
Published: SAGE Publishing 2017-10-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814017720088
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spelling doaj-5547c5c70f954955bd2321ac6592b25e2020-11-25T02:54:29ZengSAGE PublishingAdvances in Mechanical Engineering1687-81402017-10-01910.1177/1687814017720088Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control schemeYan-li Chen0Jing-chun Qin1Zhi-yan Dong2Shun-an Liu3Heng-liang Zheng4School of Mechanical Science and Engineering, Jilin University, Changchun, ChinaSchool of Mechanical Science and Engineering, Jilin University, Changchun, ChinaNetwork Control Laboratory of Electric Department, CRRC Changchun Railway Vehicles Co., Ltd, Changchun, ChinaSchool of Mechanical Science and Engineering, Jilin University, Changchun, ChinaNetwork Control Laboratory of Electric Department, CRRC Changchun Railway Vehicles Co., Ltd, Changchun, ChinaThe control scheme of a robotic coax-helicopter was investigated and a control scheme was proposed to simultaneously satisfy not only nominal performance and robust performance but also the complexity, flexibility, and computation of controller design. The complete dynamics was considered including flapping dynamics and inflow velocities. A robotic coax-helicopter dynamic model was reasonable divided into three subsystems to separately design controller based on the analysis of singularity value of the output and each inputs with fully considering the couplings. Every subsystem controller design was based on the comparisons in the performance and design complexity among the previous H ∞ loop-shaping method, the existed linear matrix inequality method, and the proposed method. A sufficient set of solvability conditions are addressed to provide a flexible performance index design for the longitudinal and lateral velocity subsystems controller. Meanwhile, the pitch–roll attitude subsystem controller was designed taking use of the previous full-order H ∞ loop-shaping method. The existed linear matrix inequality method was applied the heave–yaw subsystem because of its low computational complexity. Finally, simulations were implemented to show the effectiveness of the selection of each part’s controller law in the proposed control scheme.https://doi.org/10.1177/1687814017720088
collection DOAJ
language English
format Article
sources DOAJ
author Yan-li Chen
Jing-chun Qin
Zhi-yan Dong
Shun-an Liu
Heng-liang Zheng
spellingShingle Yan-li Chen
Jing-chun Qin
Zhi-yan Dong
Shun-an Liu
Heng-liang Zheng
Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme
Advances in Mechanical Engineering
author_facet Yan-li Chen
Jing-chun Qin
Zhi-yan Dong
Shun-an Liu
Heng-liang Zheng
author_sort Yan-li Chen
title Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme
title_short Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme
title_full Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme
title_fullStr Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme
title_full_unstemmed Multilayer hierarchical control for robotic coax-helicopter based on the H robustness and mixing control scheme
title_sort multilayer hierarchical control for robotic coax-helicopter based on the h robustness and mixing control scheme
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8140
publishDate 2017-10-01
description The control scheme of a robotic coax-helicopter was investigated and a control scheme was proposed to simultaneously satisfy not only nominal performance and robust performance but also the complexity, flexibility, and computation of controller design. The complete dynamics was considered including flapping dynamics and inflow velocities. A robotic coax-helicopter dynamic model was reasonable divided into three subsystems to separately design controller based on the analysis of singularity value of the output and each inputs with fully considering the couplings. Every subsystem controller design was based on the comparisons in the performance and design complexity among the previous H ∞ loop-shaping method, the existed linear matrix inequality method, and the proposed method. A sufficient set of solvability conditions are addressed to provide a flexible performance index design for the longitudinal and lateral velocity subsystems controller. Meanwhile, the pitch–roll attitude subsystem controller was designed taking use of the previous full-order H ∞ loop-shaping method. The existed linear matrix inequality method was applied the heave–yaw subsystem because of its low computational complexity. Finally, simulations were implemented to show the effectiveness of the selection of each part’s controller law in the proposed control scheme.
url https://doi.org/10.1177/1687814017720088
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